Special Federal Aviation Regulation

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[Federal Register: December 20, 1995 (Volume 60, Number 244)]
[Page 65831-65940]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Parts 91, 119, 121, 125, 127, and 135
[Docket No. 28154; SFAR 50-2]

RIN 2120-AF62
Commuter Operations and General Certification and Operations Requirements


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AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Final rule.
[Docket No. 28154; Amendment Nos. 91-245, 119, 121-251, 125-23, 127-45, 135-58, SFAR 50-2, SFAR 71 and SFAR 38-2]

SUMMARY: This rule requires certain commuter operators that now conduct operations under part 135 to conduct those operations under part 121. The commuter operators affected are those conducting scheduled passenger-carrying operations in airplanes that have passenger-seating configurations of 10 to 30 seats (excluding any crewmember seat) and those conducting scheduled passenger-carrying operations in turbojet airplanes regardless of seating configuration. The rule revises the requirements concerning operating certificates and operations specifications for all part 121, 125, and 135 certificate holders. The rule also requires certain management officials for all certificate holders under parts 121 and 135. The rule is intended to increase safety in scheduled passenger-carrying operations and to clarify, update, and consolidate the certification and operations requirements for persons who transport passengers or property by air for compensation or hire.


EFFECTIVE DATE: January 19, 1996.

Effective Date:
01/19/1996

Termination Date:
Until Further Notice

Addresses:

FOR FURTHER INFORMATION CONTACT: Alberta Brown, (202) 267-8321; Katherine Hakala, (202) 267-8166; or Dave Catey, (202) 267-8166; Federal Aviation Administration, 800 Independence Avenue, SW, Washington, DC 20591.
SUPPLEMENTARY INFORMATION:

Outline of Final Rule

I. Introduction
II. History
III. The Problem and Related FAA Action
A. Accident Rate for Commuter Operations
B. Public Perception
C. Congressional Hearings
D. NTSB Study
E. Related FAA Action
IV. The Proposed Rule and General Description of Comments
V. Major Issues
A. General Justification
B. Applicability
C. Aircraft Certification
D. Flight Time Limits and Rest Requirements
E. Age 60 Rule
F. Dispatch System
G. Airports
H. Effective Date and Compliance Schedule
VI. Discussion of Specific Proposals
A. Part 121 Discussion
1. Subpart E--Approval of Routes: Domestic and Flag Air Carriers
2. Subpart F--Approval of Routes: Approval of Areas and Routes
for Supplemental Air Carriers and Commercial Operators
3. Subpart G--Manual Requirements
4. Subpart H--Airplane Requirements
5. Subpart I--Airplane Performance Operating Limitations
6. Subpart J--Special Airworthiness Requirements
7. Subpart K--Instrument and Equipment Requirements
8. Subpart L--Maintenance, Preventive Maintenance, and
Alterations
9. Subpart M--Airman and Crewmember Requirements
10. Subpart N and O--Training Program and Crewmember
Qualifications
11. Subpart P--Aircraft Dispatcher Qualifications and Duty Time
Limitations: Domestic and Flag Air Carriers
12. Subparts Q, R, and S--Flight Time Limitations and Rest
Requirements: Domestic, Flag, and Supplemental Operations
13. Subpart T--Flight Operations
14. Subpart U--Dispatching and Flight Release Rules
15. Subpart V--Records and Reports
B. Part 119-- Certification: Air Carriers and Commercial
Operators
VII. Discussion of Comments Related to Costs and Benefits
VIII. Regulatory Evaluation Summary
IX. The Amendments

Background

I. Introduction

On March 29, 1995, the Federal Aviation Administration (FAA)
published a Notice of Proposed Rulemaking (NPRM) on "Commuter
Operations and General Certification and Operations Requirements"
(Notice No. 95-5; 60 FR 16230.) In Notice 95-5, the FAA proposed that
commuter operations conducted in airplanes with 10-30 passenger seats
be conducted under the domestic or flag rules of part 121 of title 14
of the Code of Federal Regulations. Currently, scheduled passenger-
carrying operations in airplanes with passenger-seating configurations
of over 30 seats or more than 7,500 pounds payload capacity are
conducted under part 121. Scheduled passenger-carrying operations in
airplanes with passenger-seating configurations of 30 seats or less and
7,500 pounds or less payload capacity are conducted under part 135.
Part 121, which provides the safety requirements for all major air
carriers (as well as for any certificate holder conducting scheduled or
nonscheduled operations with airplanes configured with more than 30
passenger seats), is generally considered to have more restrictive
requirements than part 135. The regulatory changes were introduced in
order to address the continually changing needs of the industry and to
fulfill the agency's statutory requirement. This is the final rule,
based on Notice 95-5.

II. History

Historically, the maximum certificated takeoff weight (MCTW) of an
airplane determined both an airplane's categorization and operating
requirements. Beginning in 1953, airplanes with an MCTW of 12,500
pounds or less were defined as "small airplanes" and were permitted
to carry fewer than 10 passengers in on-demand air taxi service. The
rules under which those operations were conducted were eventually
codified as part 135. Airplanes with an MCTW of more than 12,500 pounds
were defined as "large airplanes," and most large airplanes carried
20 or more passengers in scheduled air transportation. The Civil
Aeronautics Board (CAB) used the large/small dividing line to separate
major airline companies, who were required to obtain a Certificate of
Public Convenience and Necessity (CPCN) from the CAB in order to
operate in interstate commerce as a common carrier, from on-demand air
taxi operators, who were exempted from obtaining a CPCN.

During this time, the CAB issued only a small number of CPCN's to
major, publicly-recognized companies, such as Eastern, American, Delta,
Pan Am, TWA, etc. In contrast, on-demand air taxi operators numbered in
the thousands. These operators were typically fixed-base, usually at
small airports, and owned fewer than five airplanes. They provided on-
demand air transportation as well as other services, such as training
new pilots and selling and renting small airplanes. Typically, the air
taxi portion of such an operator's business was a small part of that
business and rarely involved any scheduled operations.

Beginning in the late 1960's, airplane manufacturers began to
design and build small airplanes, that is, less than 12,500 pounds
maximum certified takeoff weight, that were capable of carrying more
than 10 passengers, often close to 20. Some air taxi operators began to
offer services that resembled the services of the major airlines, given the economic opportunity to operate under the less restrictive requirements of part 135. Though
these scheduled commuter operators began to overtake some air taxi operations, they still remained a small percent of the thousands of air taxi operators.

In 1978, as a result of the Airline Deregulation Act, the airline
industry was deregulated economically and air carriers were given more
freedom to enter and exit markets without prior government economic
approval. One of the most significant effects of this deregulation was
that it allowed major carriers to eliminate service to smaller
communities, where such service proved to be uneconomical for the large
aircraft the carriers operated. Major carriers were replaced in those
communities by the commuter carriers. Under this "hub and spoke"
system, the major part 121 air carriers provided service to the large
metropolitan airports, while the growing class of scheduled part 135
air carriers provided service between smaller communities as well as
feeder service from the smaller communities to the larger cities to
connect with the major carriers' operations. With these changes, the
traditional two categories of operations became three categories of
operations--scheduled commuter operations, traditional air taxis, and
traditional major air carriers.

Also in 1978, in response to the Airline Deregulation Act, the FAA
reissued part 135 standards to upgrade commuter and air taxi safety
requirements and make them more like part 121. At that time part 135
certificate holders were required to meet more stringent requirements
in several areas, including weather reporting, flightcrew training,
maintenance, and qualifications for management personnel.

Since 1978, the FAA has issued a number of separate rule changes to
further align part 135 safety requirements with those in part 121.
Despite this realignment, differences between the regulations still
exist. The economic incentive to operate under part 135 still exists
because the requirements in part 135 are still less restrictive than
the part 121 requirements in many instances.

For the remainder of this document the following terms are used in
the following ways. "Commuter," "commuter airline," and "commuter
operator" mean those operators conducting scheduled passenger-carrying
operations under part 135 in airplanes with a passenger-seating
capacity of 30 or fewer seats. This current use of the word
"commuter" does not include scheduled passenger-carrying operations
conducted under part 121 in airplanes with a seating capacity of 31 to
60 seats. The term "commuter category airplane" used in this document
refers to airplanes type certificated in that category under part 23 in
contrast to airplanes type certificated under part 25 which are
transport category airplanes. The term "nontransport category
airplanes" is used for commuter category airplanes and SFAR 41 and
predecessor normal category airplanes to be operated under part 121, as
well as for some older airplanes certificated before the predecessors
of part 25 (parts 04 and 4b of the Civil Air Regulations) came into
existence. The Department of Transportation (DOT) uses the term
"commuter" more broadly to include all scheduled passenger-carrying
operations conducted in airplanes with a passenger-seating capacity of
20 to 60 seats. (Note: The High Density Rule, 14 CFR part 93 uses
"scheduled commuters" differently. Its meaning under that part is not
relevant to its use in this document.) The term "regional," which is
used by industry to refer to short-haul, passenger-carrying, scheduled
operations conducted under part 121 or part 135, is not generally used
by the FAA.

III. The Problem and Related FAA Action

Recent part 135 commuter accidents have focused public, government,
and industry attention on the safety of commuter operations. While the
safety level of part 135 commuter operations has continued to improve,
accident data, public perception, and recent government inquiries show
a need for additional measures.

III.A. Accident Rate for Commuter Operations

The airline industry that uses airplanes with a passenger-seating
capacity of 60 or fewer seats to conduct scheduled operations under
parts 121 and 135 is an essential part of the air transportation
network in the U.S. These airlines now fly more than all airlines did
in 1958. In 1993, over 50 million passengers, 12 percent of the total
passenger flights in the country, were flown by these airlines. Half of
these passengers were flown in part 135 operations, i.e., in aircraft
with 30 or fewer seats.

Over the past two decades the safety record of part 135 commuters
has greatly improved. The accident rate per 100,000 departures in 1993
was one-fourth the accident rate in 1980. However, the accident rate
for commuter airlines operating under part 135 continues to be higher
than the rate for domestic part 121 airlines. In the past 2 years,
several commuter airline accidents occurred that attracted media and
public attention and caused government and industry officials to
scrutinize the safety system for commuter operations under part 135.

These accidents included the December 1, 1993, crash of a Jetstream
3100, operated by Express II (as Northwest Airlink), at Hibbing, MN;
the January 7, 1994, crash of a Jetstream 4100, operated by Atlantic
Coast Airlines (as United Express), at Columbus, OH; and the December
13, 1994, crash of a Jetstream 3200, operated by Flagship Airlines (as
American Eagle), at Raleigh-Durham, NC. All of these accidents involved
fatalities.

III.B. Public Perception

With the increase in the number of flights to many communities
conducted in airplanes with a seating capacity of 30 seats or less,
some members of the public are questioning whether they are receiving
an appropriate level of safety in small propeller-driven airplanes
compared to the level of safety they receive in larger aircraft. This
public concern is partly a result of the integration of commuter
carriers with major airlines under an arrangement known as code-
sharing. The term "code-sharing" refers to the computerized airline
reservation system that lists a commuter flight in the reservation
system under the same code used by a major carrier. A passenger who
books with a major carrier may have a leg of the flight automatically
booked with a smaller commuter affiliate of the major carrier.

With the media attention to recent commuter accidents, the
passenger may also believe that the flight involves more risk because
the smaller airplane and its operation may not have to meet the same
safety standards. Most passengers probably do not realize that some
differences in standards are necessary because of differences in the
airplane and operation and that some of the accidents that are
categorized by the media as "commuter" accidents occurred in flights
that were being conducted under part 121; that is, in airplanes with
over 30 passenger seats.

The differences in regulations were initially based on differences
in the types of operations and differences in the size of airplanes;
these differences in many instances still apply. But other differences,
such as certain performance and equipment requirements, operational control requirements, and passenger information requirements are not size- or operationally-based. Some differences between the two sets of regulations must be maintained while others can be eliminated to improve the safety of commuter operations.

III.C. Congressional Hearings

On February 9, 1994, Congress held hearings on the adequacy of
commuter airline safety regulations. The purpose of the hearings was to
determine if FAA safety regulations should be modified to establish a
single standard for all scheduled operations regardless of airplane
size. Representatives of government, industry, and the public presented
testimony. Most testimony supported the upgrading of safety
requirements.

III.D. NTSB Study

In November 1994, the National Transportation Safety Board (NTSB)
published a study on commuter airline safety. (National Transportation
Safety Board Safety Study: Commuter Airline Safety, NTSB/SS-94/02.) The
study was based on the NTSB's analysis of accident investigations and
previous studies, on a recent site survey of airline operations and
policies conducted at a representative sample of commuter airlines, and
on information obtained from a public forum on commuter airline safety
convened by the NTSB.

In the study, the NTSB found that the commuter air carrier industry
has experienced major growth in passenger traffic and changes in its
operating characteristics since the NTSB's 1980 study of the commuter
airline industry. The NTSB found that there has been a trend in the
industry toward operating larger, more sophisticated aircraft, and many
carriers have established code-sharing arrangements with major
airlines. The NTSB concluded that the regulations contained in 14 CFR
part 135 have not kept pace with changes in the industry.

As a result of the findings, the NTSB issued the following safety
recommendations to the FAA:

-- Revise the Federal Aviation Regulations such that all
scheduled passenger service conducted in aircraft with 20 or more
passenger seats would be conducted in accordance with the provisions of
14 CFR part 121. (A-94-191)

-- Revise the Federal Aviation Regulations such that all
scheduled passenger service conducted in aircraft with 10 to 19
passenger seats would be conducted in accordance with 14 CFR part 121,
or its functional equivalent, wherever possible. (A-94-192)

In the 1994 study, the NTSB examined the differences in flight
dispatch requirements between parts 121 and 135. The NTSB found that,
in the absence of support from licensed dispatch personnel, it is
difficult for a part 135 pilot to accomplish several tasks between
flights in the short periods of time available. The lack of support
might increase the risk of critical mistakes that could jeopardize the
safety of flight. As a result the NTSB issued the following
recommendation to the FAA:

Require principal operations inspectors (POI) to periodically
review air carrier flight operations policies and practices concerning
pilot tasks performed between flights to ensure that carriers provide
pilots with adequate resources (such as time and personnel) to
accomplish those tasks. (A-94-193) The FAA published all of the NTSB
recommendations in the Federal Register (59 FR 63185, December 7, 1994)
and received public comments generally supporting the expansion of the
operational rules of part 121, except for flight time limitations, to
commuter operations under part 135. Some commenters had considerable
reservations about applying certain part 121 equipment requirements to
smaller airplanes. The FAA considered these comments in developing this
rule.

III.E. Related FAA Action

In December 1994, the FAA proposed revisions to the training and
qualification requirements of certificate holders conducting commuter
operations under part 135. The proposed rule also addressed crew
resource management training for pilots, dispatchers, and flight
attendants in part 121. (59 FR 64272, December 13, 1994) [Add Final
Action]

IV. The Proposed Rule and General Description of Comments

In Notice 95-5, the FAA proposed to require that all scheduled
passenger-carrying operations in airplanes with a passenger-seating
configuration of 10 or more seats (excluding any crewmember seat) and
all scheduled operations in turbojets (regardless of the number of
seats) must be conducted under part 121. The proposal would require
certificate holders now conducting scheduled passenger-carrying
operations under part 135 in airplanes with a passenger-seating
configuration (excluding any crewmember seat) of 10 to 30 seats or in
turbojets to be recertificated and to conduct the applicable operations
in compliance with part 121 requirements. In some instances the
proposed rule revised the requirements of part 121 to make compliance
with the requirements feasible for operations in smaller, nontransport
category airplanes.

In response to Notice 95-5, the FAA has received over 3,000
comments from the public. Of these, most are solely on the issue of the
Age 60 Rule. Many of the Age 60 commenters are pilots and other
individuals who address the current rule in part 121; very few address
the specific Age 60 issue contained in this rulemaking, i.e. the
applicability of the Age 60 Rule to pilots of affected commuter
airplanes. These comments are summarized in Section V.E., The Age 60
Rule.

Approximately 200 comments were received on the substantive issues
raised by Notice 95-5. These commenters represent air carriers;
manufacturers; associations representing air carriers, manufacturers,
pilots, dispatchers, and passengers; State and local governments; the
U.S. Small Business Administration; the National Transportation Safety
Board; and individuals. While some commenters voice general support for
the goals of Notice 95-5, most raise concerns about specific proposals.
Industry commenters are particularly concerned about the costs of
complying with the proposed rule.

The FAA also conducted three public meetings on the proposed rule:
on May 18, 1995, in Anchorage, Alaska; on June 14, 1995, in Chicago,
Illinois; and on June 21, 1995, in Las Vegas, Nevada. Testimony from
the public meetings and written statements submitted at the meetings
have been included in the FAA public docket, have been considered by
the FAA in developing the final rule, and are discussed in the
following discussion of comments along with all written comments that
were submitted to the FAA docket.

In Notice 95-5, the FAA identified major issues that the agency
addressed in developing the proposal. These included applicability of
the proposal, aircraft certification issues, flight time limits, the
Age 60 Rule, use of a dispatch system, certain equipment items, and the
compliance schedule. Comments received on these major issues and the
FAA's response to these comments are discussed in Section V. Comments
received on specific proposals and the FAA's response to these comments
are discussed in Section VI. Comments specifically addressing cost
issues are discussed in Section VII. Below is a list of some of the
major commenters and their associated abbreviations. The full name of
each commenter is used when the commenter is first mentioned. In
subsequent discussions, the commenter's abbreviation, as shown below,
is used.

Abbreviations for Commenters

AAAE American Association of Airport Executives
AACA Alaska Air Carriers Association
ADF Airline Dispatchers Federation
AIA Aerospace Industries Association
ALPA Air Line Pilots Association
APA Allied Pilots Association
ASA Atlantic Southeast Airlines
GAMA General Aviation Manufacturers Association
HAI Helicopter Association International
IAPA International Airline Passengers Association
NACA National Air Carrier Association
NATA National Air Transportation Association
NTSB National Transportation Safety Board
Penair Peninsula Airways
RAA Regional Airlines Association

V. Major Issues

V.A. General Justification

In Notice 95-5, the FAA justified the proposed rule on the basis of
the higher accident rate for commuter airlines. Parts of the proposed
rule were also supported by the testimony from Congressional hearings
on commuter airline safety regulations and by the NTSB study, based on
accident investigations and previous studies, which found that part 135
regulations had not kept pace with changes in the industry.

Comments: The NTSB and the Air Line Pilots Association (ALPA)
generally support the proposal and its justification. A comment from
the International Airline Passengers Association (IAPA) supports the
rulemaking justification by stating the findings of a recently
completed IAPA study of commuter/regional airplane safety records in
the United States covering the period 1970 through March 31, 1994.
According to IAPA, during that period carriers using airplanes with 30
or fewer seats had 29 fatal accidents with 249 passenger fatalities;
over 30 seat regional carriers had 1 fatal accident with 2 passenger
fatalities; major airlines had 11 fatal domestic jet accidents with 527
passenger fatalities.

In contrast to these comments, many other commenters state that the
proposed rulemaking lacked sufficient justification. Recent accident
data, say these commenters, have shown significant reductions in
accident rates for commuters so that the difference in accident rates
for part 121 operations and part 135 commuter operations is minimal.
According to at least one of these commenters, if the accidents that
occurred in extreme environments such as Alaska are removed, the
accident rate under the two parts would be either the same or lower for
part 135 commuter operations.

According to some commenters, the recent accidents cited in Notice
95-5 were all caused by pilot error and thus would not have been
prevented by this rulemaking but could have been prevented by
improvements in training.

Some commenters state that the proposed rule is the result of
public, media, and agency overreaction to recent commuter accidents and
that both the public and the media drew inaccurate conclusions about
commuter airline safety from these accidents. According to these
commenters, instead of hastily proposing rules based on incomplete
information, the agency should have informed the public that many so-
called commuter operations are already being conducted under part 121.

Several commenters state that the proposed rule will decrease
safety because in order to avoid the proposed restrictions, certificate
holders now operating airplanes with a seating capacity of 10 to 19
passenger seats will switch to reciprocating-powered airplanes with a
passenger seating capacity of 9 or less in order to continue to operate
under part 135. Furthermore, some commenters state that if fares are
significantly increased to pay for the more restrictive requirements,
passengers may choose ground transportation, which has a much higher
accident rate.

Several commenters state that the proposed rule would have a
significant economic impact on small airline operators, in some cases
forcing them to close their businesses, thus eliminating air
transportation to some locations. In addition, according to some
commenters, the proposed rule would have a negative impact on
competition, particularly in the foreign market because the cost of
U.S. manufactured airplanes would increase.

FAA Response: The FAA does not agree with the assessment that the
proposed rule lacked sufficient justification. The FAA recognizes the
validity of some of these comments especially in regard to unintended
safety decrements if the aircraft performance portions of the proposed
rule were adopted on the schedule proposed. While the FAA recognizes
the improvements in the accident data for commuter airlines in recent
years, it intends through this rulemaking, and other related rulemaking
actions underway, to reduce the accident rate even further.

Several commenters have questioned the need for a rule that would
move affected commuters into part 121 domestic or flag operations. For
instance two commenters argue that a dispatch system would not have
prevented the three accidents cited by the FAA in the NPRM. It would be
a mistake to assume that the FAA is basing this final rule on just
those three accidents. Similarly, it would be a mistake to conclude
that the FAA is justifying this rule on merely "perceptions" of a
problem. Those accidents were catalysts for the Government to focus on
the differences in the part 121 accident rate and the accident rate for
10- to 30-seat part 135 commuters. Over the next 15 years affected
commuters are expected to have had 67 more accidents than they would
have had if the accident rate for part 135 affected commuters were the
same as that for part 121 scheduled operators. The FAA believes that
adoption of this rule will significantly close the accident rate gap
over time.

The FAA believes that the part 121 regulatory scheme for scheduled
operations is more appropriate for the 10- to 30-seat scheduled
operations. The added safety features and requirements in part 121
domestic/flag rules, including the dispatcher system, will increase
safety for the affected commuters. Because most accidents are caused by
human errors, rules such as the part 121 training rules and the
dispatcher system rules are some of the most valuable tools in reducing
the number of these kinds of accidents. Rules that most directly relate
to preventing accidents caused by human errors are being imposed on the
affected commuters on a faster schedule than many of the other rules
(e.g., aircraft performance and certain equipment retrofits). It can be
reasonably anticipated that applying part 121 operating rules,
including these two groups of rules, can begin to immediately and
significantly reduce the accident rate for affected commuters. For
instance, the FAA anticipates that requiring operators to have someone
(i.e., a certificated dispatcher) double check the work of the pilot
and provide the flight crew with updates on weather and alternate
airports can reduce some human factor errors. The FAA believes that if
the flight crew is subjected to more stringent flight and duty
safeguards (either the current part 121 domestic flight and duty rules
or the rules in a soon to be issued NPRM in which the FAA will propose
to overhaul all the flight and duty regulations), the dangers of
fatigue causing a human factors error will be reduced. Enhanced part
121 training (which is being required of affected commuters in an
associated final rule) will also reduce some human factor errors.

It is critically important to impose the bulk of the part 121
regulatory scheme on affected commuters because the absence of any
significant portion of that regulatory scheme may lessen the
effectiveness of the rest of the safety features in the part 121
regulatory scheme. Even the best trained and well rested pilot is a
human being and, therefore, subject to making errors. With a dispatcher
system, the chances of pilot miscalculations or oversights could be
reduced. Moreover, a dispatcher can assist the flight crew in making
enroute plans for an alternate airport (which might be necessary due to
weather problems, air traffic control problems, airplane equipment
problems, fuel problems, etc.) while the crew focuses on flying the
airplane. It is reasonable to conclude that the accident rate for
affected commuters can be reduced to a level closer to that of current
part 121 domestic operations by eliminating most of the regulatory
differences that the two different regulatory schemes allowed.

While major air carriers may require commuter affiliates to follow
certain part 121 standards, and in some cases even exceed some part 121
standards, no part 135 commuter operator currently operates under part
121 operations specifications or totally complies with all part 121
standards (e.g., many part 121 requirements are based on the assumption
that transport category airplanes are operated). Most importantly, no
part 135 commuter is required by current FAA regulation to comply with
part 121 requirements.

Recent accidents brought to public attention the differences
between part 135 and part 121 and the lack of continuing justification
for these differences. As Notice 95-5 pointed out, the distinction
between these two types of operations was, in the beginning, an obvious
necessity. Major air carriers engaged in public transportation were
entirely different from the small on-demand, air taxi operator. But
with the development and growth of what has come to be known as
commuter service, the line between the two has blurred. Certain
segments of the commuter industry have continued to develop commuter
category airplanes, holding the line at 19 passenger seats in order to
stay within the limits of the less restrictive airworthiness
regulations for nontransport category aircraft. This has created the
potential for the further development of commuter airplanes
specifically designed to stay within the limits of the less restrictive
regulations while at the same time becoming as sophisticated or more
sophisticated in technology than some transport category airplanes
operated by the major carriers. With hindsight, the FAA may not have
drawn the line as it currently is but would have attempted from the
start to maintain one set of requirements.

Until now the line between the requirements has not created a
safety concern, but as the commuter market grows, the disparity between
the two sets of requirements is of more concern. There is no longer any
justification for maintaining two sets of standards for scheduled
operations in airplanes with a passenger-seating configuration of 10 or
more seats. When a passenger pays for a ticket on an FAA certificated
commuter operation, that passenger must be assured of the highest
possible level of safety.

With respect to commenters concerns that the proposed rules will
actually decrease safety because certificate holders will switch to
reciprocating-powered airplanes, the FAA has modified the proposal,
especially in regard to the schedule for some airplanes to meet part
121 airplane performance criteria, to allow operators sufficient time
to build up capital or credit to make changes to the existing fleet or
to purchase new airplanes that meet the higher performance standards.
The FAA does not want to move so fast as to force operators to use
airplanes that have even higher accident rates (i.e., airplanes with 9
or fewer seats).

The FAA finds that safety and the public interest require extending
the proposed compliance dates for imposing part 121 performance
criteria requirements and some equipment requirements until it is
economically feasible for operators of 10- to 19-seat airplanes to
acquire or lease replacement aircraft. The FAA has analyzed the
situation and has concluded that many operators of 10-15 seat aircraft
would replace those aircraft with 9 or fewer seat aircraft to avoid the
sudden imposition of large costs on their current fleets. Without the
FAA modifying its proposal with regard to airplane performance
requirements, many airplanes would be eliminated from scheduled service
at the first compliance date (i.e., 15 months after publication of the
final rule) and operators of other airplanes would have to offload
passenger seats, thereby causing the economic and safety impacts
discussed previously. This modification would be consistent with the
National Transportation Safety Board's (NTSB) recommendation for
airplanes with 10- to 19-seats in scheduled service. For those
aircraft, the NTSB recommended that scheduled passenger service be
conducted in accordance with part 121 "* * * or its functional
equivalent, wherever possible".

Clearly the NTSB used the phrase "wherever possible" because it
knew that it was not possible for a substantial portion of the 10- to
19-seat airplane fleet to meet all of the requirements of part 121. The
NTSB carefully chose its words when it made its recommendations for 10-
19 seat airplanes used in scheduled service. The NTSB recognized that
the FAA necessarily had to exercise judgment about which part 121
regulations to impose, which regulations could be modified to achieve
functional equivalency, and which regulations simply might not be
possible.

In regard to comments that higher fares resulting from this
rulemaking will cause passengers to switch to less safe modes of
transportation, it has been the FAA's observation that passengers are
usually willing to pay for safety. While some may choose to drive
rather than fly, that has not stopped the airlines in the past from
raising fares. It should also be noted here that the public tolerates a
higher accident rate for automobile travel than for airplane travel. If
air transportation accident rates approached that of ground travel,
most Americans would stop flying. The air transportation industry is
very aware of this; it is the main reason that air transportation is
safe. As one commenter points out, the recent commuter accidents caused
a 12 percent drop in passengers on commuter airlines. That is a
significant cost to industry.

The FAA has carefully considered the economic impact of the
proposed regulations and has reviewed and revised its analysis in light
of the comments received. (See Section VIII.) The agency has determined
that the impact of the final rule should not disrupt air transportation
service and that few, if any, certificate holders will discontinue
their commuter operations. During the transition period, the FAA will
work with certificate holders who are switching to part 121
requirements to make the switch as smooth as possible. It should also
be noted that the compliance schedule provides for a gradual updating
of equipment and operations and will allow certificate holders the
choice of upgrading or phasing out airplanes that cannot be upgraded
without significant cost.

Some may argue that there may still be limited circumstances, even
with these changes, where the effects of this rule (and related
rulemakings on upgraded training requirements and pilot flight time and duty
limitations) will be so burdensome as to lead to adverse safety
consequences and/or a loss of critical air service. This is neither
FAA's intention nor its expectation. Indeed, the entire premise of this
rulemaking is that safety standards can and must be improved for the
benefit of passengers in 10-30 passenger seat aircraft in scheduled
service.

Nevertheless, there is in place in 14 CFR 11.25 a process for
requesting and granting exemptions from regulatory requirements,
including those adopted here. As with any request for exemption, of
course, an applicant would have to demonstrate that the public interest
justifies such an exemption. In this case, an applicant could show, for
example, that it is unable to comply with a particular provision or a
particular schedule date due to circumstances beyond its reasonable
control (rather than its own failure to act in a timely or prudent
manner), that there is convincing evidence that alternative service is
unavailable to the public, and that the carrier would be able to
maintain an adequate level of safety during the period of the requested
exemption.

We would expect that any exemption from this rule would be for a
limited period only, such as the time required for delivery of a piece
of equipment that has been ordered. Our goal would be to permit the air
carrier to come into compliance with the rule in an orderly manner, and
not simply to delay or avoid the cost of compliance.

The FAA considers this rulemaking a positive step towards promoting
air transportation by renewing confidence in commuter operations. Most
importantly, this rulemaking should reduce the accident rate of the
affected commuters to a rate that is closer to that of current part 121
domestic operators.

This rulemaking is consistent with the FAA's obligation in
accordance with section 44701(d) of Title 49 of the U.S. Code that when
prescribing a regulation or standard to promote safety or to establish
minimum safety standards, the Administrator shall consider the duty of
an air carrier to provide service with the highest possible degree of
safety in the public interest. The intent of this rulemaking is to
provide the highest possible degree of safety to affected commuter
operations.

V.B. Applicability

The FAA proposed that part 121 requirements would apply to all
scheduled passenger-carrying operations for compensation or hire in
airplanes with a passenger-seating configuration of 10 or more seats
and to all scheduled passenger-carrying operations for compensation or
hire in turbojet-powered airplanes regardless of seating capacity.
(Throughout the rest of this document these certificate holders are
referred to as the "affected certificate holders" or the "affected
commuters.") Under the proposal, scheduled passenger-carrying
operations in non-turbojet airplanes with 9 or fewer passenger seats,
on-demand operations with airplanes with 30 or fewer passenger seats,
operations in single-engine airplanes, and operations in rotorcraft
would continue to be under part 135.

The proposed rule would also have eliminated the frequency of
operations test of five round trips per week which allowed some part
135 scheduled operations to be conducted under the on-demand rules of
part 135.

Comments: While no commenters specifically object to applying part
121 requirements to commuter operations in airplanes of 20 to 30
passenger seats, several commenters, many of them small part 135
certificate holders, object to applying part 121 requirements to
commuter operations in airplanes of 10 to 19 passenger seats. According
to these commenters, the FAA did not sufficiently justify imposing the
more restrictive part 121 requirements on operations in these size
airplanes and the small certificate holders of these airplanes would
not be able to meet the economic burden of the proposal. A few
certificate holders state that if the regulations are implemented as
proposed they would either have to downgrade their airplanes, reduce
the number of passenger seats, or terminate certain services. This is
especially the case for small fixed-based certificate holders, who
conduct mostly on-demand service with some scheduled service, and for
certificate holders who service remote areas such as parts of Alaska,
Hawaii, or the islands of Samoa.

Commenters also state that the burden is greater for certificate
holders not affiliated with a major airline and that drawing the line
at 10 or more includes many small, independent certificate holders.
According to commenters, these certificate holders provide a different
kind of service from what the larger commuter operators provide.

One commenter, IAPA, states that part 121 requirements should apply
to all scheduled passenger-carrying operations, no matter how many
seats are on the airplane. According to this commenter, by leaving out
the under 10-seat aircraft from the rulemaking, passengers would be
exposed to travel on the least safe aircraft operating in scheduled
passenger transportation. According to the commenter, most under 10-
seat aircraft are piston-engined, with a lower level of engine
reliability and performance. The aircraft are frequently operated in
harsh environments thereby exposing passengers to higher risks.

Many of the commenters who object to the applicability of part 121
to aircraft with 10 to 19 passenger seats, also object to the
definition of "scheduled" in proposed Sec. 119.3. According to these
commenters, the effect of the current description in SFAR 38-2 of
commuter air carriers that includes 5 round trips per week should not
be changed. Apparently some small certificate holders that conduct
mostly on-demand service also provide one or two scheduled service
flights per week. According to these commenters, if they have to
upgrade the airplanes and operations to part 121 to conduct these
scheduled flights, they will downgrade the airplanes or terminate the
service. The commenters state that they cannot afford to comply with
part 121, that the service they provide offers one-of-a-kind service to
remote places or resorts, and that in some instances there is no ground
transportation to these locations.

Several on-demand operators and the National Air Transportation
Association (NATA) comment that the FAA should not revise part 135 on-
demand requirements either at this time or at any time. These
commenters are responding to a statement in Notice 95-5 that additional
standards for on-demand air taxi operations may be considered in the
future.

The General Aviation Manufacturers Association (GAMA) objects to
including all scheduled passenger-carrying operations in turbojets
under part 121 regardless of the number of passengers. While GAMA
agrees with the FAA's assumption that no turbojets are being used in
regularly scheduled part 135 operations, it objects to the
applicability because the FAA presented no technical justification for
the proposal. GAMA recommends allowing turbojets with a passenger-
seating capacity of 9 or less to operate under part 135. Aerospace
Industries Association (AIA) also objects that no rationale was
presented for including turbojets. AIA states that the proposed rule
offers an unfair competitive advantage for normal category turboprops
against jets with a passenger-seating capacity of 9 or less. United
West Airlines states that it is a small operation with two jets, that
it costs $70,000 a year to train its four pilots, and that the proposed
rule will put the airline out of business.

Two individual commenters recommend that "any scheduled operation
with airplanes seating more than 9 passengers but less than 19
passengers" be operated under supplemental rules when that scheduled
operation is a code-sharing arrangement with another part 121 scheduled
carrier.

FAA Response: The so-called "frequency of operation" provision in
the SFAR 38-2 definition of commuter air carrier does not exist for
current part 121 operations. Affected commuters being upgraded to part
121 by this rule will be required to conduct all of their scheduled
operations under part 121 regardless of the number of scheduled
operations. However, the FAA has decided to retain the frequency of
operations distinction for those operations conducted in airplanes with
a passenger-seating configuration of 9 seats or less by revising the
definitions of "commuter operation" and "on demand operation" in
Sec. 119.3. Therefore, scheduled operations in airplanes with a
passenger-seating configuration of 9 or less (except turbojets) and
conducted on a particular route with a frequency of fewer than five
round trips per week (regardless of whether one or more airplanes are
used on the route) would be conducted under the requirements applicable
to on-demand operations.

The FAA believes that, because of the nature of the operation in
which small turbojets, which are type certificated under part 25, are
used (e.g., transoceanic, long range, international, etc.), they
approximate the operations of larger air carriers. For example, part
135 contains no requirements for long-range navigational equipment or
long-range fuel considerations. In an effort to increase the safety for
passengers carried in those kinds of operations, the FAA has determined
that any scheduled operations of turbojet airplanes should be conducted
under part 121.

The FAA disagrees with commenters who suggest that commuter
operations in code-sharing arrangements should be conducted under the
rules for supplemental operations. Code-sharing, although it may affect
passengers' perceptions, is a business/marketing arrangement and is not
the basis for an FAA regulatory scheme. Scheduled operations in
airplanes with 10 or more passenger seats should come under part 121
domestic or flag, as appropriate, not under supplemental rules.

The only operators who currently operate under part 135 on-demand
rules that would be required to conduct their operations under part 121
scheduled rules are those who are included because, as discussed above,
part 121 does not contain a frequency of operation provision. If
circumstances in the future necessitate a change to these rules,
commenters will have an opportunity to comment on any proposed changes.

Air Tour Industry Comments: Several comments were received from air
tour operators in the State of Nevada and the vicinity of the Grand
Canyon. Some of these certificate holders would be affected by the
rulemaking because they operate nontransport category airplanes of 10
to 19 seats and because they provide point-to-point service; for
example, from Las Vegas to Grand Canyon Airport even though the flights
are exclusively marketed as sightseeing and not point-to-point travel.
Despite the fact that they technically fall into the category of a
commuter operator, these commenters claim that they are more like an
on-demand operator and that the proposed rule would penalize them for
using larger, safer airplanes than their competitors. One of these
commenters states that it does not fly city to city, but flies
regularly scheduled flights that take off and land at the same airport.
This operator states that, because of the nature of the operation and
because of the proposed definition changes, it would be required to
comply as a scheduled operator.

According to the commenters, since they have upgraded from 6- to 9-
seat airplanes to 19-seat airplanes, they have been required to install
ground proximity warning systems (GPWS), traffic alert and collision
avoidance systems (TCAS), cockpit voice recorders (CVR), and flight
data recorders (FDR), while their competitors have not been burdened by
these costs. According to some of these commenters, this equipment is
not beneficial in their operating environment because they typically
fly in VFR conditions on short-range flights of an hour or less.

The commenters complain that if the proposed rule is implemented,
they will be forced to replace the turboprop airplanes with smaller
reciprocating-powered planes and will thereby lose some significant
safety benefits such as the following:

-- The two-pilot crew requirement with captains required to
hold an Air Transport Pilot rating.

-- Aircraft certificated to higher levels of aircraft
performance.

-- Aircraft maintenance procedures under the more
comprehensive Continuous Airworthiness Maintenance Program.

-- Safety equipment such as GPWS, TCAS, CVR, and weather
radar.

One commenter lists some of the more "onerous" proposed
requirements:

-- "Ditchable" exits in case of water landings.
-- Emergency floor path exits.
-- Third attitude indicator (in aircraft flown in daylight
under visual flight rules).
-- Portable protective breathing equipment (PBE).

A commenter points out that the new aircraft performance
requirements would limit maximum operating weight at Grand Canyon due
to the high altitude.

According to these commenters, switching to smaller airplanes will
increase air traffic congestion in the Grand Canyon area, decrease
safety for passengers, and double or triple noise levels.

According to one commenter, these certificate holders do not have
code-sharing partners and while these certificate holders sometimes
provide point-to-point service, the flights are typically part of an
all-inclusive tour package which includes ground transfers to Las Vegas
hotels, sightseeing flights to the Grand Canyon, and motor coach tours
of the Grand Canyon. This is totally unlike typical commuter
operations.

Another commenter, however, says that at least one of the air tour
operators does use code-sharing with a major carrier and that the
offering of its scheduled flights is available by referencing airline
computers all over the world.

Some of the commenters cite an NTSB report ("Safety of the Air
Tour Industry in the United States," June 1, 1995) which states that
the implementation of SFAR 50-2 has created a safe operating
environment for air tour operators over the Grand Canyon. One commenter
quotes NTSB as saying, "The level of safety of air tour operations
could be improved by creating a national standard for air tour
operations that contains definitions specific to the air tour industry
and specific requirements, including unique operations specifications,
to accommodate localized unique conditions, similar to the special
conditions contained in SFAR 50-2."

One commenter states that his company recruits retired airline
pilots to provide a high level of experience and stability to the
flightcrews.

The Clark County Board of Aviation is concerned that the proposed
rule could be devastating to individual certificate holders and
adversely affect the vitality of the air tour industry in Southern
Nevada.

The Grand Canyon Air Tour Council states that the proposed expanded
definition of "scheduled operations" is the problem and that the
definition was changed with no satisfactory explanation or
justification.

The Office of the Lieutenant Governor of Nevada testified at the
public meeting held in Las Vegas that compliance would affect a "$250
million industry that we have worked hard to develop."

FAA Response: The FAA does not agree that air tour operations are
totally unlike commuter operations. Much of an air tour flight is like
much of a commuter flight. If an air tour operator is conducting
scheduled operations, as defined in Sec. 119.3, in airplanes with a
passenger-seating configuration of 10 or more, it must comply with part
121 domestic or flag requirements, as applicable. This includes
operators who fly from and return to the same point on a scheduled
basis.

The FAA agrees that certain aspects of air tour operations make
them appear to be unlike commuter operations. For example, portions of
air tour flights are at lower altitudes, typically over rugged and
remote terrain, and often in airspace that is congested with other
sightseeing aircraft. The FAA has begun an air tour industry project to
study the implications of these differences to safety and to develop
regulations, as necessary, to address specific features of air tour
operations. If regulations are implemented as a result of the project,
they would be in addition to current regulations, as is SFAR 50-2 which
prescribes requirements for special conditions relating to flights over
the Grand Canyon. The FAA project will consider the recent NTSB study
cited by commenters. Because certain part 121 and 135 provisions are
being recodified into part 119, SFAR 50-2 and SFAR 71 are being updated
to conform to this rulemaking.

Alaskan Comments: Several comments were received from certificate
holders in Alaska, Alaska government agencies, and others interested in
how the proposal will affect Alaskan operations. Currently Alaskan
certificate holders conducting scheduled operations in airplanes of 10
to 30 seats comply with part 135. The regulations allow them not to
comply with flight time limitations for scheduled operations
(Sec. 135.261(b) and (c)) and instead allow them to follow the
regulations for on-demand operations. Alaskan certificate holders using
airplanes of more than 30 seats must comply with part 121 supplemental
requirements for nonscheduled flights and flag requirements for
international and intra-Alaska scheduled operations. Notice No. 95-5
proposed no exceptions for Alaska. Certificate holders whose operations
fit the applicability for scheduled operations for airplanes of 10 or
more seats would be required to comply with part 121 domestic
requirements. International operations would follow flag requirements
of part 121 and charter operations would follow supplemental
requirements of part 121. Alaskan operators currently operating under
part 121 flag rules would have to operate under part 121 domestic rules
except for those operations that meet the definition of flag operations
in proposed Sec. 119.3.

The basic thrust of the comments is that the Alaska environment is
unique and that requiring Alaskan commuter operators to comply with
part 121 requirements would be devastating to certain certificate
holders in Alaska and therefore to certain segments of air
transportation. Furthermore commenters point out that most air
transportation in Alaska is conducted in small reciprocating-powered
airplanes with passenger-seating capacities of under 10 seats.
Therefore, the proposed rule would not have a significant effect on air
transportation safety in Alaska and would impose an economic burden on
a few certificate holders who provide upgraded, i.e., safer, service.
According to commenters, the accident rate for airplanes with under 10
seats is much higher than for turbine-powered airplanes with 19 seats.
(Accident data analyzed by the FAA verifies that, unlike the rest of
the nation, the part of the commuter fleet in Alaska involved in
accidents contains a large proportion of under-10-seat aircraft.)

Peninsula Airways (Penair), as well as other commenters, states
that characteristics of Alaska make commuter operations in the State
unlike those in other parts of the country. In particular flights are
conducted in the same time zone, pilots do not have long commutes to
their jobs, flights are not usually conducted between 9 p.m. and 7
a.m., and operations subject to Air Traffic Control (ATC) are not in
congested airspace. This rationale is primarily in defense of using the
flight time limit requirements of part 135 nonscheduled operations.

Several commenters emphasize the absolute necessity of air travel
in Alaska where many of the towns and villages are not accessible by
road. They say that Alaskans are dependent on air transportation and
the cost of that transportation must remain affordable. High cost items
in the proposal, such as the possible need to upgrade airports, the use
of a dispatch system, the various equipment requirements, and certain
performance requirements, would boost the fares to levels that many
residents of Alaska could not afford. The State of Alaska Department of
Transportation and Public Facilities states that "the proposed air
carrier and airport regulations could devastate Alaska's heavily
aviation dependent economy."

The Alaska Air Carriers Association (AACA) states that the proposed
rule would end the growth of the 10- to 19-seat airplane and would
increase fares by 67 to 100 percent. The proposed airport legislation
is expected to cost the state $100 million. AACA states that the
proposed rule would directly affect only 15 certificate holders in
Alaska. Two-thirds of the scheduled air carriers use aircraft with a
seating capacity of 10 seats or less.

ERA Aviation, which currently operates under part 121 flag rules,
objects to the proposal to operate as domestic/supplemental. It
operates over 100 aircraft, fixed and rotary wing, nationally and
internationally. The commenter states that for years Alaska part 121
operators have been operating under flag rules, both for scheduled and
nonscheduled operations. This has allowed increased flexibility in crew
scheduling, which is necessary because of the length of Alaska routes,
the lack of facilities in remote locations, and the lack of road
networks or other alternate forms of transportation to outlying
communities. Section 119.21 would require these carriers to operate
under domestic rules, which would decrease crew scheduling flexibility,
add substantially to costs, derogate safety, and probably result in the
elimination of vital air transportation services to some outlying
communities. The commenter says there is no safety justification for
such a change because Alaska part 121 operators have established an
excellent safety record under existing rules. They say that, at the
very least, Alaska carriers currently operating under flag rules should
be allowed to continue to operate under flag rules for both scheduled
and nonscheduled operations.

A part of the proposal that would have affected several Alaskan
certificate holders is the proposal that single-engine airplanes with
10 passenger seats now operating scheduled flights under part 135 would
in effect have to remove a seat in order to continue operating in
scheduled service under part 135. Single-engine airplanes are
ineligible for operation under part 121. The only 10-seat single-engine
airplane model involved is the single-engine de Haviland DHC-3 Otter
(not to be confused with the twin-engine de Haviland DHC-6 Twin Otter
mentioned elsewhere in this notice). According to AACA and other commenters,
there is no possible safety benefit in taking a seat out of an
airplane, but the cost to certificate holders who want to continue to
use these airplanes in scheduled operations will be significant.

NATA comments that no accident involving the Otter would have been
prevented by limiting the seating to 9 passengers. Furthermore,
according to the commenter, the FAA cost on this issue is another
example of gross underestimation; actual costs will be 15 times higher
(almost $22,000 per aircraft). The City and Bureau of Juneau opposes
the proposal to remove a seat from the 10-seat airplanes so that they
can operate under part 135. This commenter notes that there will be
additional flights, additional noise, and additional congestion on the
water and in the air. It notes that it is incomprehensible how the
reduction of one seat from the Otter will provide an additional level
of safety. Wings of Alaska comments that the most cost-efficient
floatplane used in southeast Alaska is the single-engine DHC-3 Otter.
Because there is no cost-effective replacement aircraft available for
float operations that offers the same capacity as the Otter, replacing
them is not an option. Wings states that it operates the Otter about 6
months a year. Four communities that do not have runways receive daily
service. Wings purchased five 10-seat Otters in '92-93 to improve
service to a wilderness sports facility, substantially reducing noise
by reducing the number of flights by 50%. Wings notes that considering
initial operating experience (IOE) and route check requirements, it is
being operated at a higher level of safety than the 10 seat, on-demand
aircraft allowed under the rule to be operated in part 135. Wings
estimates that the removal of one seat would have cost them $85,000 in
1994. Wings asks that the Cessna Caravan and the Cessna Grand Caravan
also be allowed to operate with 10 seats. AACA comments that Ketchikan
Air Service, Taquan Air Service, and Wings of Alaska together operate
12 Otters in southeastern Alaska.

The NTSB comments that it intentionally excluded airlines that
operate exclusively in Alaska from its study of commuter airline safety
because of the unique characteristics of the environment in Alaska. The
NTSB currently is conducting a study of commercial Alaska aviation
including commuter airlines. The NTSB held two public meetings in
Alaska during June 1995 and visited a number of scheduled and
nonscheduled part 135 certificate holders to collect information for
the study. The NTSB intends to compare flying operations in Alaska with
the rest of the U.S. The study is scheduled for completion in 1995.
Several other commenters mention the study and suggest that the FAA
should wait until the study is completed before making any changes to
Alaskan regulations.

ALPA, GAMA, and other commenters state that safety issues are the
same in or out of Alaska and that, therefore, Alaska should not be
given a blanket exemption from the rulemaking. ALPA and GAMA state that
Alaskan certificate holders, as well as certificate holders in other
parts of the country, may need to be exempted from certain requirements
that are not applicable to the type of operations being conducted and
should go through the standard exemption request procedures in such
cases.

One comment from an individual pilot in Alaska states that the
schedule he flies of 14 days on and 14 days off is exhausting, and that
even though he gets 10 hours of rest in each 24 hours, it is not enough
over a 14-day period. He is in favor of the proposed flight time limit
changes.

Some Alaskan certificate holders comment that they rely on
experienced pilots who are familiar with the particular demands of
Alaskan operations. Penair states that 10 percent of its pilots are age
60 or over and that 20 percent are over age 52.

Commenters who oppose the rule suggest either exempting Alaska
altogether, not including the 10-to-19 seat airplanes in the rule, or
allowing under-19-seat airplanes to be covered under the supplemental
rules of part 121 rather than the domestic rules.

FAA Response: The FAA agrees with the commenters who state that
safety issues are the same in or out of Alaska. The FAA has
specifically considered the implications of the proposal on Alaska
given its unique characteristics and has determined that the rules
should apply to Alaska as proposed. While the NTSB comment on Notice
95-5 states that the NTSB excluded Alaska from its safety study on
commuter airline safety, the NTSB states in the report that its
findings from the information obtained in the course of the study
"apply to operations in Alaska as well as the other 49 states and U.S.
Territories." ("Commuter Airline Safety," NTSB/SS-94/02). Therefore,
this final rule does not provide a blanket exemption for Alaska.

In response to the single-engine airplane issue, the FAA has
decided to allow an exception to continue. Currently, several part 135
certificate holders conduct scheduled passenger-carrying operations in
single-engine airplanes type certificated with two pilot seats in the
"cockpit" and 9 passenger seats in the "cabin." Some certificate
holders are authorized to conduct scheduled operations in that
airplane, the DHC-3 Otter, under daytime VFR, and carry a tenth
passenger in the right-hand pilot seat. In Notice 95-5, the FAA
proposed to limit all scheduled operations of single-engine airplanes
to the carriage of nine passengers, under all conditions. (60 FR 16235,
16273) The FAA has decided to allow the current practice to continue
for operators who currently conduct single-engine operations under
daytime VFR with a tenth passenger.

Comments on Exemptions/Deviations/Waivers: Currently some
certificate holders operating under part 135 that will be affected by
this rulemaking have obtained exemptions, deviations, and waivers from
certain part 135 requirements.

AACA states that AACA has held an exemption on behalf of its
members allowing removal and installation of aircraft seats by certain
pilots and trained ground personnel under an FAA-approved program. The
commenter states that it is unclear whether or not aircraft operated
previously under part 135 in Alaska would be allowed to continue this
seat removal and installation under part 121 with an appropriate
exemption. AACA states that taking away this option would significantly
increase air carriers' costs and diminish their flexibility to utilize
aircraft in "combi" (combination cargo/passenger) configurations.
AACA recommends that all exemptions, deviations, or waivers held by a
part 135 operator automatically be carried over into its part 121
operation. As presently written, Notice 95-5 would require compliance
with part 121 first, and only then would the FAA evaluate requests for
exemptions to part 121 rules. This places additional and unwarranted
operational costs on air carriers transitioning to part 121.

FAA Response: The specific exemption referred to by the AACA
applies only to operations with airplanes with a passenger-seating
configuration of 9 or less, and therefore is not affected by this
rulemaking.

However, exemptions issued for operations under part 135 do not
automatically continue in effect for operations under part 121.
Therefore, affected commuters who will in the future be operating under
part 121 must reapply for any exemptions they believe should apply to
their part 121 operations after the compliance date of this rule. Also,
general exemptions issued to present part 121 operators will
not apply automatically to new part 121 operators so any new part 121
operator will have to apply to be included in these existing
exemptions.

V.C. Aircraft Certification

The proposed rule would amend part 121 to require each 10- to 19-
passenger seat airplane that is to be operated in scheduled operations
and for which an application for type certification is made after March
24, 1995, to be type certificated in the transport category. Affected
commuter airplanes are type certificated under the requirements of part
23.
In Notice 95-5 the FAA stated its intent to review the standards of
parts 23 and 25 to see if the level of safety intended by part 25 could
be achieved for those airplanes with a passenger-seating configuration
of 19 or less through compliance with a particular standard of part 23
or another standard, in lieu of the corresponding standard of part 25.
On completion of that review the FAA stated its intent in future
rulemaking to consider amending part 25 as necessary to accommodate
type certification in the transport category of certain types of
airplanes previously type certificated in the commuter category.

The FAA also proposed that airplanes configured with 10 to 19
passenger seats already in service or manufactured in the future under
an already existing part 23 commuter category type certificate would
have to comply by specified compliance dates with certain performance
and equipment requirements in part 121. These performance and equipment
requirements are discussed later in this preamble.

In Notice 95-5 the FAA included a table that set out a list of
potential modifications that were being considered for application to
airplanes having a passenger-seating configuration of 10-19 seats that
were type certificated in the commuter category (or a predecessor) if
the airplanes are to be used in scheduled operations under part 121.
The table included a column that indicated that for 12 of the 38 issues
addressed, the FAA had determined that any required upgrade should
apply only to airplanes manufactured under a type certificate for which
application is made after March 24, 1995. Since these 12 issues will be
the subject of a future NPRM, the FAA is not addressing specific
comments on the substance or cost of these issues in this document.

Comments: ALPA fully supports the proposal to require newly-
designed airplanes to comply with the standards of part 25 and also
supports continued use of commuter category airplanes. The commenter
does not, however, concur that airplanes type certificated under part
23 normal category (i.e., pre-commuter category) should be permitted to
remain in operation with more than 10 passenger seats, even in non-air
carrier service. ALPA appears to base its position on differences in
performance requirements between commuter category and the predecessor
normal category standards.

American Eagle supports the proposed rulemaking and states that,
"while there may be limited circumstances when aircraft design and/or
manufacture may preclude or delay compliance with FAR part 121 or FAR
part 25, cost and weight considerations should not be an acceptable
barrier to the increase in safety which is derived from applying the
higher standards of aircraft airworthiness, airline operations and
passenger safety which those regulations provide."

In contrast, six other commenters do not believe that any
propeller-driven airplanes with 10 to 19 passenger seats should be
required to meet the transport category standards of part 25. Although
the commenters' reasons vary, the comments focus on three basic issues:
(1) Commuter category standards are appropriate for airplanes of this
class; (2) there is no evidence that safety would be enhanced by
requiring future airplanes to comply with part 25; and (3) the cost of
complying with part 25 would be prohibitive.

Similar comments concerning recertification of existing part 23
airplanes under part 25 were also offered, apparently under the
misunderstanding that airplanes already type certificated, or
derivatives of those airplanes, would have to be recertificated under
part 25.

Some commenters believe that the airplane certification issue is of
such magnitude that it should be held in abeyance for a separate future
rulemaking program. In this regard, the commenters assert that
extensive changes to part 25 would be needed to accommodate the
airplanes otherwise certifiable under part 23 commuter category and
that those changes would entail a considerable expenditure of FAA
resources. They further believe that any such changes should be subject
to harmonization with corresponding standards of the European Joint
Aviation Requirements (JAR).

Several commenters cite the FAA's 1977 proposal to require all
airplanes used in air carrier service to meet part 25 transport
category standards. That proposal was later withdrawn. According to
commenters, the part 23 standards of that era were considerably
different from those of today's part 23 commuter category. The level of
safety expected by the public today is much greater than that tolerated
in 1977.

A number of other commenters address the proposed retrofitting of
existing part 23 normal and commuter category airplanes to meet certain
part 25 standards. Those comments are addressed in the section-by-
section portion of this preamble (Section VI).

One commenter has developed and produces a unique propulsion system
in which two turbine engines drive a single propeller through a common
gearbox. In addition to the installations already being made in
existing airplanes, the commenter anticipates a future installation of
this system in an airplane of entirely new design. Since any new model
would have to be type certificated under the provisions of part 25 in
order to be eligible for operation under part 121, the commenter
requests that part 25 be amended to accommodate airplanes with this or
similar propulsion systems.

FAA Response: Rather than forcing the retirement of part 23 normal
category airplanes, as recommended by ALPA, the FAA proposed in Notice
No. 95-5 to permit their continued use in air carrier service provided
certain changes were made on a retrofit basis to enhance their level of
safety. Banning those airplanes would be extremely costly, but most
importantly could result in an unintended safety decrement. Indeed, the
FAA's analysis indicates that moving too quickly on the imposition of
part 121 standards could have the unintended effect of lowering the
level of safety because operators would not be in a financial position
to quickly obtain new airplanes and currently there are not enough
replacement airplanes available that meet the higher standards. The
result could be a shift from 10- to 19-seat turbopropeller airplanes to
9-seat or less reciprocating engine airplanes, which have an even
higher accident rate.

The six commenters' assertions that commuter category standards of
part 23 are appropriate for airplanes of this class and that there is
no evidence that safety would be enhanced by type certification under
part 25 are, to a certain extent, correct. Through a number of recent
amendments and pending amendments, the level of safety established by
the commuter category has been and is being enhanced considerably. In
many instances, commuter category airplanes must meet standards that
are the same as, or very similar to, those of part 25 transport
category. Requiring future 10- to 19- passenger seat airplanes to be
type certificated under part 25 would complete this effort to ensure
that these airplanes used in air carrier service meet the same aircraft
certification standards as the larger airplanes.

In response to comments that part 23 airplanes could not be type
certificated using part 25 standards, the FAA notes that it did not
propose in Notice No. 95-5 that part 23 normal or commuter category
airplanes presently in operation would have to comply with part 25
standards for type certification. Instead, it proposed that part 23
airplanes that will be required to be operated under part 121 will have
to comply with certain part 121 equipment and performance requirements.

In response to the individual comment on a unique propulsion
system, although the commenter's request is beyond the scope of this
rulemaking, it will be considered during the review of part 25
discussed above.

V.D. Flight Time Limits and Rest Requirements

The FAA proposed that the part 121 domestic flight time limits and
rest requirements would apply to affected commuter operators when
conducting operations within the United States. Under the proposal
affected commuter operators, when conducting operations to or from the
United States, would comply with the flag flight time limitations and
rest requirements of subpart R. Additionally, if these certificate
holders use these same airplanes for nonscheduled operations, those
certificate holders would be required to comply with supplemental
flight time limitations and rest requirements of subpart S of part 121.

As stated in Notice 95-5, since the flight time limitations and
rest requirements for flag and supplemental operations were not updated
in 1985 when domestic limits were, the FAA has developed an NPRM that
is being issued concurrently with this final rule. (See elsewhere in
this issue of the Federal Register.)

Comments: Atlantic Southeast Airlines (ASA), Regional Airlines
Association (RAA), and Big Sky Airlines comment that the FAA should
provide specific and scientifically-based data to support this
significant change. Fairchild Aircraft adds that the additional time
off duty provided by the proposal will not necessarily be used for
rest. NATA comments that there are differences in part 135 operations
that justify a different set of flight time limitations and rest
requirements: part 135 operations are generally confined to a
particular area, pilots of smaller certificate holders rarely commute a
long distance to and from work, and pilots have fewer overnight stays
as part of their schedules. Air Vegas comments that unless an exception
is provided, seasonal operators would have to hire additional crews in
order not to exceed the 7-day limit of 30 hours or the monthly limit of
120 hours. This commenter notes that short-term employment of such
pilots is next to impossible. Morton Beyer and Associates comments that
the cost of hiring additional pilots is expected to add another $250
million to airline costs. Twin Otter International comments that the
1,200 yearly limit in part 135 is based on the part 121 100-hour-per-
month concept, and that the regulations really are similar.

Several individuals strongly urge the FAA to adopt the part 121
standards for the upgrading commuter pilots. American Eagle comments
that it applies part 121 domestic rules to its part 135 operations and
believes that all air carriers providing commercial passenger service
should use either the domestic or flag rules of part 121.

One individual notes that the reduced rest provision in part 135
allows for only 8 hours of rest between scheduled flights. Another
individual comments that commuter pilots have a high frequency of
takeoffs and landings, fly in the busier low-altitude airspace, deal
with more controllers per flight mile, and deal with more weather than
their part 121 counterparts. One person comments that certificate
holders routinely schedule 3-4 hour breaks to preclude violations of
the 8 hours of flight in 24 hours rule; however, the effect of this is
to stretch out the duty day. The result is a higher duty time to flight
time ratio which is not accounted for in the current rules. IAPA
supports the proposal but also expresses concern that the current
regulations fail to count, as part of duty time, the time period when
flightcrews are on reserve duty, standby duty, or carrying a pager or
other telephonic device. IAPA urges the FAA to treat reserve or standby
duty as duty time.

ALPA comments that while the upgrade to part 121 will result in an
improvement in flight time limits and rest requirements, part 121 will
continue to be deficient in this area until additional rulemaking
action is taken, as promised by the FAA.

Alaska commenters argue for maintaining the current regulations.
ERA Aviation estimates that if the proposed rule is adopted, it would
necessitate at least a 15% increase in the number of pilots it would
need, resulting in a $500,000+ increase in costs. Penair finds four
reasons for excepting Alaska: Operations are conducted in the same time
zone, few Alaska pilots commute to their jobs, less than 5% of Alaska
operations occur between 9:00 p.m. and 7:00 a.m., and Alaska does not
have the congested ATC operations which are found in the lower 48
states. AACA also presents this argument, adding that going from 1,400
hours of duty per year down to 1,000 represents a 29% decrease in
productivity. Other Alaska certificate holders, e.g., Wings, Northern
Air Cargo, Taquan Air Service, Tanana, endorse the AACA comment.

One individual commenter from Alaska opposes any attempt to create
exceptions to the requirements for Alaska. This person supports the
assertion that Alaskan operations are basically the same as state-side
operations and should be afforded no special exemptions.

This individual, a pilot who flew over 1,300 hours last year,
states that there were many consecutively scheduled 14-hour duty days
and many canceled days off. Ten hours of rest may sound adequate, but
not for days on end. The individual questions the logic that one is
more rested in one geographic area than in another. According to the
commenter, duty cycles that are unsafe in the lower 48, are also unsafe
in Alaska.

Another individual from Alaska states that the FAA has shown no
data to indicate any problem with the provisions of Sec. 135.261(b),
which allows Alaskan scheduled operators to use Sec. 135.267. The
individual states that in 1994, he flew 1320 hours, had 173 days off,
slept in his own bed every night, and never had less than 10 continuous
hours of rest in any 24-hour period. He believes he probably had more
rest and time off than the average long-haul part 121 pilot. The
commenter states that the proposed flight/duty time limits would cause
scheduling nightmares for operations in rural/remote parts of Alaska.

FAA Response: The FAA is holding in abeyance a final decision on
the proposed imposition of current part 121 flight time limitations and
rest requirements on affected commuters pending a review and
disposition of comments on the separate flight and duty rulemaking in
which the FAA proposes to overhaul all the flight and duty rules. The
separate rulemaking, if adopted, would harmonize flight and rest
requirements for all part 121 and part 135 carriers. The FAA
anticipates that the separate rulemaking will result in a net cost
savings to the industry as a whole. In the meantime, affected commuters
will continue to operate under the current part 135 flight
and duty rules. This will prevent needless expenditure
of resources by affected commuters who would have
to implement flight and rest provisions under the commuter rule
proposal and then later might have to change their system to comply
with the separate rulemaking. For the same reasons the FAA will allow
part 121 certificate holders operating in Alaska and Hawaii to continue
to follow the flight and duty rules of part 121 applicable to flag
operations, even though under this rulemaking these certificate holders
are now classified as conducting domestic operations.

Accordingly, Secs. 121.470, 121.480, and 121.500 include an
exception for affected commuters allowing that they continue to comply
with flight time limits and rest requirements of part 135.
Additionally, Sec. 121.470 will allow existing Alaska and Hawaii
intrastate scheduled domestic operations to continue to be conducted
under flag rules.

V.E. Age 60 Rule

Section 121.383(c) prohibits a certificate holder from using the
services of any person as a pilot, and prohibits any person from
serving as a pilot, on an airplane engaged in operations under part 121
if that person has reached his or her 60th birthday. Part 135 has not
had any such limitation. The FAA proposed to impose one age limitation
on all pilots employed in part 121 operations, including those pilots
currently employed in affected part 135 scheduled operations. The FAA
stated in Notice 95-5 that if it determines that it is appropriate to
propose a different age limit in another rulemaking action, it will
propose to apply the revised limitation to all part 121 operations,
including the pilots in commuter operations.

Comments: The age limitation question was the subject of over 2,000
written comments (including about 1,000 postcards from members of an
airline pilot organization) and oral presentations at public meetings.
The overwhelming majority of these comments concern the general
question of whether there is a need for an age limit in part 121, and
do not address any particular aspects of applying an age rule to
commuter pilots.

Several commenters, however, state that if commuter pilots are
subjected to an age limit, the FAA should adopt a phased-in
implementation schedule to avoid abruptly ending the careers of pilots
who had not planned on retiring at age 60. Another commenter states
that it hires over-age-60 retired part 121 pilots.

FAA Response: As discussed above, the FAA has identified a strong
need to enhance the safety of commuter operations. Commuter airlines
are carrying an increasing number of passengers over an increasing
number of miles. While safety has improved over the past two decades,
commuter airlines operating under part 135 continue to have a higher
accident rate than domestic part 121 airlines. The FAA can no longer
justify most distinctions between parts 121 and 135 commuter
operations.

The part 121 regulatory scheme provides a network of safety
features. Because most accidents are caused by human error, rules
designed to enhance the performance of pilots are among the most
valuable in reducing the number of accidents. Elsewhere in this
preamble the FAA discusses other provisions that serve this purpose,
such as the critical role of the aircraft dispatch system in double
checking the work of the pilot and providing updates on weather and
alternate airports. The training requirements for commuter pilots are
being upgraded, and eventually part 121 flight and duty time rules or
the newly proposed rules will apply to them. The Age 60 Rule provides
an additional measure of safety by reducing the risk that age-related
degradation will affect pilot performance. A pilot may have the best
training in the world, and be well-supported by an aircraft dispatch
system, but if the pilot suffers from a subtle age-related degradation
in performance, safety will be reduced. Also, the potential safety
benefits of training and dispatching may be reduced by human safety
lapses that could occur or do occur more frequently with age.

The "Age 60 Rule" was adopted by the FAA in 1959 (24 FR 9767,
December 5, 1959). At the time Notice 95-5 was issued, the FAA was also
considering whether, in the interest of safety, the Age 60 Rule should
be retained as is or revised to allow pilots to continue to fly in part
121 operations past their 60th birthday. The FAA completed its review
of the Age 60 Rule. In a Disposition of Comments (Disposition)
published in the Federal Register, [cite], the FAA announced that it
will not propose to change the Age 60 Rule at this time. The
Disposition thoroughly discusses the various issues regarding the need
for an age limitation and what that age should be, including the issues
raised in the comments to Notice 95-5 that concern the Age 60 Rule in
general, and those comments will not be further discussed here. This
rulemaking deals only with the application of part 121 rules to
affected commuter operations.

In Notice 95-5 the FAA proposed a general compliance date (that is,
a date on which most provisions must be complied with) of 1 year after
publication. The Notice also proposed delayed compliance dates for
several of the requirements (other than the age limitation), to provide
time for the work necessary to comply with the proposed requirements.
In this final rule, the FAA has adopted a general compliance date of 15
months after the date of publication of this final rule in
Sec. 121.2(c), and also has adopted delayed compliance dates for a
number of requirements, giving the air carriers 2, 4, or more years to
comply with certain of the new requirements.

In response to the comments requesting delayed compliance dates,
and after further evaluation, the FAA has considered that there are
factors warranting delay in the compliance date for the Age 60 Rule, as
it applies to those affected commuters that now will be brought under
part 121. The lack of an age limitation in part 135 has created
reasonable expectations on the part of both the affected commuter
operators and pilots regarding the length of time that the pilots would
continue in service: Some of those operators have spent money to hire
and train pilots with the expectation that they would serve past the
age of 60; and the pilots have not had to plan on leaving their
positions at age 60. In fact, certain affected commuters appear to have
a practice of hiring retired part 121 pilots, and will no longer be
able to do so.

Further, this rule requires the affected commuters to make
extensive changes in equipment, personnel, and procedures before the
general compliance date. Also, final rules have been adopted that
impose new requirements for training, including standardized pilot
training and crew resource management training. The affected commuters
operators should not be required to stop using the services of their
over-age-60 pilots in scheduled operations (10 or more seats) and train
replacements until these new programs are in place, and the training
can be under the new programs.

Accordingly, the FAA has determined that the Age 60 Rule, as it
applies to certain pilots, should have an extended compliance date. As
it applies to pilots newly hired by commuter operators, the Age 60 Rule
will apply on the general compliance date indicated in Sec. 121.2(c).
Until that date, there will be no age restrictions on the pilots of
commuter operations that are upgrading to part 121. After that date, the
affected commuters will no longer be able to hire pilots who have
reached their 60th birthday (except for pilots who as of that date were
employed as pilots for another affected commuter). However, pilots who
are employed by affected commuters on that date will be able to
continue to serve until December 20, 1999, after which the Age 60 Rule
will apply to every pilot under part 121.

The delay in applying the rule will provide some relief from the
difficulties discussed above. The 4-year compliance period for these
pilots will permit the affected commuters to recover services for
several more years from those pilots in which they recently have
invested in training. Delaying the application of the rule to new hires
until the general compliance date will give affected commuters time to
adopt new hiring practices, at a time when the operators will have many
other new requirements under this rule to comply with. The 4-year
compliance period for pilots will give them time to plan for retirement
or for changing jobs. It will also give affected commuters additional
time to make careful selections of well-qualified pilots and train them
under the new training requirements. And, the operators will not have
to replace all of their over-age-60 pilots at once, at a time when so
many other new requirements must be complied with.

V.F. Dispatch System

Parts 121 and 135 require certificate holders to exercise
operational control over all flights conducted by the certificate
holder. "Operational control" is defined in 14 CFR part 1 as "The
exercise of authority over initiating, conducting and terminating a
flight." Operational control consists of making decisions and
performing activities on an ongoing basis that are necessary to operate
specific flights safely. These activities include among other things
crew and airplane scheduling, reviewing weather and NOTAM's (Notices to
Airmen), and flight planning.

Parts 121 and 135 provide for three general types of operational
control systems based on the kinds of operations and the complexity of
operations: aircraft dispatch, flight following, and flight locating
systems. Part 121 domestic and flag operations require a dispatch
system, part 121 supplemental requires a flight following system, and
part 135 requires a flight locating system for any flight for which a
flight plan is not filed. In Notice 95-5, the FAA proposed that the
affected commuters would be required to have a dispatch system.
Affected commuters would have to meet all part 121 dispatch
requirements, including dispatcher qualification requirements,
recordkeeping, and flight release requirements. As proposed, affected
commuters that would conduct some nonscheduled flights under part 121
supplemental rules could use a flight following method for the
nonscheduled flights.

The FAA also stated in Notice 95-5 that Alaskan operations pose
certain unique problems and requested comments on alternatives that
could be considered for Alaska.

Comments: Two individuals suggest that the use of a dispatcher and
dispatch system be an option for 10- to 19-seat certificate holders,
recommending compliance with existing subpart F of part 121. Both
commenters believe that the FAA should seriously consider permitting,
at least on an interim 36-month basis, compliance with subpart F flight
following requirements in lieu of subpart E dispatch requirements for
transition carriers. This will, in their opinions, gain the early
momentum of the industry by making it possible for many certificate
holders to transition early. A long lead time is necessary to qualify
existing personnel as dispatchers under existing part 65. The
commenters remind the agency that during the early 1980's, by the FAA's
own rules, 20- to 30-seat aircraft were subject to part 121
supplemental rules, including the flight following requirements of
subpart F. One of these individuals also states that interim compliance
with subpart F flight following requirements would ease the transition
to subpart E dispatch requirements for affected certificate holders.

NATA comments that the FAA lacks understanding on the types of
operations 10- to 19-seat certificate holders typically fly and
recommends a flight following system instead of a dispatch system. NATA
states that many small, independent carriers operating aircraft with 10
to 19 seats may have only 2 to 4 of these types of airplanes and may
operate them over only a few selected routes. According to NATA, many
of these carriers conduct on-demand operations in addition to their
scheduled activity. NATA believes, along with several other commenters,
that for operations such as these, to implement a full dispatch system
will result in significant cost with little or no benefit.

RAA and other commenters suggest that the FAA identify specific
safety objectives in requiring a dispatch system for short-haul
certificate holders.

One commenter believes that a formal dispatch system for all
scheduled air carriers should be required, but points out both the pros
and cons of requiring such a system. This commenter, as well as others,
states that pilots may be shouldering many additional responsibilities
other than flying the aircraft in an effort to minimize the cost of
flight operations. Due to the task saturation of pilots and other
crewmembers, functions involving flight planning, weather analysis, and
weight and balance calculations may not be thoroughly performed.
According to the commenter, the majority of commuter pilots are, as a
rule, very young and inexperienced. These crews must continually
perform at peak levels of performance both on the ground and in the
air.

According to this commenter, as well as others, the use of the
flight dispatcher would increase safety, operational efficiency, and
productivity. The duties of filing the flight plans, checking NOTAMs,
planning fuel requirements dictated by weather, and obtaining ATC
routing would be completed by the dispatcher prior to the crew arriving
for the flight. Optimum routes based on known ATC or weather delays
would be filed, resulting in substantial fuel savings and improved
arrival and departure reliability. The pilots would now be able to
concentrate on flying and be able to relax and rest between flights.
Flight could be more effectively managed, thus saving fuel, maximizing
aircraft utilization, and passenger satisfaction.

On the other hand, according to the commenter, mandating the
dispatch system for part 135 air carriers may create some heavy
financial burdens. It will require a facility, communications hardware
for the facility and the aircraft, trained personnel, and training for
dispatchers. The initial capital outlay would not be recovered for
several years. According to the commenter, this mandate will place
severe constraints on many less established carriers and may actually
result in bankruptcy for some.

Many commenters are in favor of the role of the aircraft dispatcher
in operational control issues. One commenter states that the
requirement for a formal dispatch system is long overdue.

One commenter believes that dispatch centers might create a sense
of complacency on the part of the flightcrew and, along with other
commenters, thinks that automated flight planning and flight following
information should be used in lieu of dispatchers and dispatch centers.
Two of the commenters advocating automated flight following systems state
that the three accidents cited by the FAA in Notice 95-5 would not have
been prevented by the use of a dispatcher. One commenter states that in
his experience PIC's typically check dispatcher computations but do not
duplicate the computations as the FAA stated in Notice 95-5.

The NTSB states that in its 1994 study report, it examined the
differences in flight dispatch requirements between parts 121 and 135.
The NTSB found that, in the absence of support from licensed dispatch
personnel, pressures on commuter airline pilots to accomplish several
tasks between flights in shorter periods of time might increase the
risk of critical mistakes that could jeopardize the safety of flight.
As a result, the NTSB recommended that the FAA require each principal
operations inspector (POI) to periodically review air carrier flight
operations policies and practices concerning pilot tasks performed
between flights. This review was to ensure that carriers provide pilots
with adequate resources (such as time and personnel) to accomplish
those tasks. According to NTSB, the proposed rulemaking, if
implemented, would meet the intent of the safety recommendation (A-94-
193).

ASA, RAA, and Gulfstream International Airlines support many of the
elements of the dispatcher rule. They state that flight dispatch
systems that are required under part 121 are extensive since they
address the dispatch and en route communications needs for a span of
air carriers from international airlines with worldwide flight
operations to the largest U.S. regional carriers. ASA supports the
requirement for licensed dispatchers, believing that the most qualified
candidates for licensing as dispatchers are the individuals currently
employed as flight followers. These commenters request that the
criteria in Sec. 65.57 be examined to provide guidance for granting a
dispatcher certificate based on practical experience as a flight
follower under part 135 operations. According to the commenters, many
flight followers have passed the written portion of the dispatch
license but have not attended formal dispatch school and do not hold
licenses. However, they may have extensive practical experience in
scheduled air carrier operations performing what is essentially a
dispatcher function. According to these commenters, the criteria
contained in Sec. 65.57 includes experience in scheduled military
operations. The commenters believe that if military experience is
applicable, the experience of a flight follower with a scheduled
airline should qualify. These commenters also point out that the
practical portion of the dispatcher license is administered using a
Boeing 727 aircraft. The commenters believe that while many of the
functions and decision making circumstances would be the same, the
experience of part 135 flight followers, managing flights of high
performance turbopropeller-powered aircraft is a considerably more
significant and practical measure of their capabilities than military
experience or demonstrating their skills in managing a turbojet
operation. The commenters believe that the cost and time to send
current flight followers to a formal dispatcher school is not
justified.

Samoa Air comments that since its longest flight is only 70 miles
(35 minutes), a dispatch system would not enhance or change any of its
current requirements. Samoa has established VFR and IFR fuel
requirements to all of its destinations and the requirements do not
change. The only alternate airport is the destination airport. Samoa
also states that Sec. 121.101 requires each domestic and flag operator
to show that enough weather reporting facilities are available along
each route to ensure weather reports and forecasts necessary for
operations. Section 135.213 allows the pilot in command to use various
other sources, including his own weather assessment, for VFR
operations. Of the four airports Samoa serves, only one (departure
airport) is in controlled airspace with weather reporting facilities
and instrument approach procedures. Enroute and terminal weather
conditions are received through the ATC tower from their weather
station. VHF communications with the tower cover almost the entire
route, so the aircraft has ready access to any weather information
available and direct information on the status of communications,
navigation, and airport facilities. A dispatcher would not enhance
safety but would add significant cost. If Samoa is required to provide
weather conditions at each airport to the pilot from an approved source
and the pilot can not assess the weather himself, the rule change could
eliminate all of Samoa's present operations.

Similarly, Inter Island and Air Vegas comment that the requirement
for enroute weather reporting is unfeasible because of minimal weather
reporting facilities in the certificate holders' regions. Air Vegas
also comments that radio communication in mountainous terrain would be
difficult if not impossible with VHF radio systems because mountains
block radio transmission.

Air Vegas comments that all "dispatcher duties" are currently
being accomplished by personnel in the operations department, station
managers, and company pilots. All flight following is being done by
telephone. The commenter states that current flight following
procedures meet part 135 requirements and are operationally safe and
efficient.

Mesa Airlines comments that due to its short flight segments and
the lack of significant weather changes in the areas in which it
operates, a dispatch system is not needed. Mesa believes that all
enroute communications can be accomplished by ATC.

AACA states that the requirements of subpart E come at a time when
the availability of weather information in Alaska has been identified
as a significant issue adversely affecting aviation activities
(proceedings of an NTSB "Aviation Safety in Alaska" forum, May 1995).

The Airline Dispatchers Federation supports the dispatch proposal
and agrees with the upgrading of current commuter facilities to
dispatch centers. It believes this upgrading is necessary because of
the extensive use of code-sharing by the aviation industry. The
commenter is not in favor of amending part 121 dispatch rules for
certificate holders of the 10- to 19-seat category. The commenter
provides its estimate of costs to certificate holders that could be
affected by the implementation of this rule. The commenter notes that
the costs provided by some certificate holders may not be accurate. For
example, cost estimates concerning flight planning and performance
issues are inaccurate since several airlines use bulk stored flight
plans and performance information taken directly from aircraft flight
manuals for fuel planning. The commenter also provides its assessment
of various aircraft accidents for which it believes dispatchers could
have made a difference in changing events that led to the accident
(crew fatigue, lack of management oversight, operational control
issues, late arriving weather information).

ALPA comments that dispatchers should be required to complete their
5-hour inflight operating experience in 10- to 30-seat aircraft, not in
larger 60-seat aircraft, as currently allowed. ALPA proposes that
Sec. 121.400(b) be amended by adding a group specific to propeller-
driven aircraft with a seating capacity between 10-30 seats.

AACA comments that due to the operating environment of Alaska, the
pilot and not the dispatcher is in a better position to access
and evaluate operational control information.
The commenter believes that scheduled operations in Alaska more closely
resemble the operations conducted under supplemental rules and not
domestic or flag operations. The commenter notes that pilots frequently
are not in radio communication with company offices directly, but could
communicate via Flight Service Station, ATC, or other aircraft.
According to the commenter, enroute and destination weather conditions
are either not accessible or not available at any time from
"official" sources. The commenter notes that three affected
certificate holders in Alaska presently have a part 121 type dispatch
system in place. AACA further states that the assumption that estimated
fuel savings by dispatchers would offset the cost of establishing a
dispatch system is not true. AACA recommends that the FAA adopt the
flight following supplemental rules of part 121 for Alaskan 10-19 seat
certificate holders. AACA also recommends that current part 135
personnel be "grandfathered" for dispatcher certificates if they have
been employed as flight followers. The commenter notes that the
practical experience dealing with turboprop aircraft and flight
planning may be lost to the industry if flight followers are required
to take extensive dispatcher training courses, pass a written and
practical test, and lose time and money on the job while they obtain an
FAA dispatcher certificate.

FAA Response: The FAA anticipates that requiring operators to have
a certificated dispatcher double check the work of the pilot and
provide the flightcrew with updates on weather and alternate airports
can reduce human factor errors. With a dispatcher system, the chances
of pilot miscalculations or oversights could be reduced. Moreover, a
dispatcher can assist the flightcrew in making plans for an alternate
airport (which might be necessary due to weather problems, air traffic
control problems, airplane equipment problems, fuel problems, etc * *
*) during the flight while the crew focuses on flying the airplane.

The FAA disagrees with the recommendation to make the use of a
dispatcher and dispatch system optional since that would not address
the safety issues involved. The FAA also disagrees that a flight
following system is an acceptable alternative to a dispatch system or
that dispatch systems are not needed for limited flight distances if
there is adequate weather reporting facilities. The use of a dispatch
system is based on the type of operation (scheduled), and not the
distance of a flight, the number of aircraft, or the type of aircraft
being flown. Flight following systems are used for nonscheduled
operations, and could be used for nonscheduled operations by affected
commuters under the supplemental rules of part 121. Note: The dispatch
system requirements apply only to scheduled passenger-carrying
operations.

The FAA disagrees with the basic idea that the decision making
process of operational control of aircraft can be made by automated
means. While automation has improved the accuracy and timeliness of
flight planning, weather information, and NOTAMs, nothing so far has
replaced the decision making capabilities of a certificated dispatcher.
Dispatchers receive training in subject matter beyond just flight
planning, e.g. crew resource management, hazardous materials
regulations. These subjects are just a small representation of the
subject matter an aircraft dispatcher must know in order to make
operational control decisions.

The FAA agrees with the comment that dispatchers are usually in a
better position to review weather reports and forecasts than pilots
hurrying to accomplish other postflight/preflight aircraft duties.
Operational control issues are enhanced when both the pilot in command
and the aircraft dispatcher are jointly responsible for the safe
conduct of a flight. As several commenters point out the overall level
of safety is enhanced when a dispatcher is available to assist and back
up the pilots who already may have numerous responsibilities in
addition to flying the airplane. Thus, while it may not be possible to
pinpoint accidents that have actually been prevented by a dispatch
system, there can be little doubt that the existence of a dispatch
system contributes to the overall high level of safety of scheduled
operations under part 121.

The FAA does not agree that use of dispatchers would lead to
complacency on the part of the flight crewmembers. Section 121.663
states that for each domestic and flag operation, a dispatch release
must be prepared based on information furnished by an authorized
dispatcher. The pilot in command and an authorized dispatcher shall
sign the release only if they both believe that the flight can be made
safely. Dispatchers provide the necessary resources and expertise
needed to review operational control issues.

In response to comments that in some companies "dispatch"
functions are being adequately performed by individuals from three
separate departments (operations, station managers, and company
pilots), the FAA finds that operational control decisions can not be
effectively made by three separate groups of individuals. The
perception is that "whoever is available" makes the decision. For
effective operational control, the dispatch process should be
standardized and consistent.

In response to NATA's and others' comments on the nature of 10- to
19-seat certificate holders, the FAA finds that these certificate
holders are not unique. The same situation currently exists for some
part 121 certificate holders who are required to maintain dispatch
systems.

In response to comments on the issue of limited areas of operation
and short flight duration, the requirement for a dispatch facility is
not based on distances, the type of aircraft, or weather patterns
alone. It is the type of operation (scheduled) an air carrier is
currently operating under that determines if dispatch systems are
required. The role of the aircraft dispatcher in the operational
control of aircraft provides an enhancement to safety that has clearly
been established through years of operations by many air carriers in
both domestic and flag operations. Continuous communications could be
accomplished with HF radios or through satellite communications, both
of which can be provided through vendors.

The FAA agrees with commenters that for some part 135 certificate
holders, personnel will first have to acquire the necessary certificate
and then complete required air carrier training requirements for
dispatchers. The average dispatcher school curriculum lasts 5 weeks and
usually includes instruction on both the written and practical tests.
The FAA believes that some part 135 personnel already possess aircraft
dispatcher certificates and that these personnel would be required to
attend only the air carrier's dispatcher training program. Regardless,
once an air carrier employs a certificated dispatcher, company training
would have to be completed. That training would entail 40 hours of
basic indoctrination, differences training, initial ground/transition
of 30-40 hours (based on the type of aircraft), and a competency check
(see Sec. 121.422).

While the FAA does not agree with AACA's recommendation to
"grandfather" dispatcher certificates to current flight followers or
flight locating personnel, Sec. 65.57 outlines a means of providing
credit for previous experience in order to take the practical test. All
dispatcher applicants must complete the appropriate written and
practical tests before a certificate can be issued. The FAA agrees that
training costs will be incurred to prepare current flight following or
flight locating personnel to qualify for a dispatcher certificate,
regardless of who pays for the training. Replacement personnel will be
needed if the decision by the certificate holder is to send current
employees to dispatcher training.

There is no requirement for dispatchers to attend a formal school.
Section 65.57, entitled experience requirements, allows several options
in lieu of a formal school.

In response to specific requests to expand the criteria in
Sec. 65.57 (aircraft dispatcher experience requirements) to include
personnel assigned to flight locating and flight following under part
135, the FAA believes that some part 135 experience is acceptable as
equivalent experience in Sec. 65.57. Through current policy and
guidance provided to FAA inspectors, a review on a case-by-case could
be accomplished to ascertain if an applicant has equivalent experience.

In response to comments on the current format of the dispatcher
practical exam, Sec. 65.59 requires an applicant for an aircraft
dispatcher certificate to pass a practical test with respect to any one
type of large aircraft used in air carrier operations. Further, current
practical test standards require dispatcher applicants to exhibit
adequate knowledge of applicable aircraft flight instruments and
operating systems. The scope of the practical test allows for turboprop
aircraft and representative commuter operations. Practical tests are
developed by the inspector conducting the test and can be designed for
any type of large aircraft, including turboprop airplanes.

There is only one dispatcher written examination, the Airline
Transport Pilot question book. The selection sheet has questions
applicable only to dispatchers and not based on any particular make and
model of aircraft. The FAA is considering developing written tests
geared to commuter-type operations. However, the current written exam
is valid in that it tests for areas common to all make and models of
aircraft. The test requires knowledge of various subject areas, i.e.
the ability to interpret weather information, interpret regulations,
handle emergencies, compute weight and balance, etc.

The FAA disagrees with the ALPA recommendation to require
dispatchers to receive 5 hours of operating experience in aircraft they
will actually dispatch. Section 121.463(c) requires the dispatcher to
satisfactorily complete at least 5 hours of operating familiarization
in one of the types of airplanes in each group he is to dispatch.
Section 121.400(b) includes all sizes of propeller-driven aircraft
under group 1. Therefore, the FAA allows dispatchers to complete the
operating familiarization in airplanes that are not exactly the same
size or configuration as the ones they will dispatch.

V.G. Airports

Section 121.590 requires that no air carrier or pilot conducting
operations under part 121 may operate an airplane into a land airport
in the U.S. (or territory, etc.) unless the airport is certificated
under 14 CFR part 139. Section 135.229 states that no certificate
holder may use any airport unless it is adequate for the proposed
operations.

Part 139 prescribes regulations governing the certification and
operation of all land airports that are served by any scheduled or
nonscheduled passenger air carrier operating airplanes with a seating
capacity of more than 30 passengers. The FAA's authority is limited by
statute (49 U.S.C. 44706(a)) to the 30-passenger-seat dividing line.
The FAA, in conjunction with the Department of Transportation, has
sought legislation that would grant the agency the authority to
certificate any airport that receives scheduled service by a
certificate holder utilizing airplanes designed for 10 or more
passenger seats.

Accordingly, pending Congressional resolution of this issue,
affected commuters are permitted to operate into other than part 139
certificated airports. If the FAA receives expanded authority over
airport certification, it would propose rulemaking standards that are
sufficiently flexible to cover the range of airports presently served
under part 135.

Comments: Nine comments were received on this issue, with the major
concern being that airport legislation currently being considered may
include requirements that some communities may not be able to afford
which would negatively affect air service to these communities.

The Las Vegas Department of Aviation comments that it has purchased
and upgraded satellite airports in the Las Vegas area to help relieve
the congestion at the McCarran International Airport. The commenter is
concerned that the Clark County Department of Aviation, the Grand
Canyon Tour Operators, and the Las Vegas Department of Aviation may not
be able to afford additional airport upgrades. This would cause
certificate holders that currently operate out of the non-certificated
outlying airports to move their operations back to McCarran, thereby
increasing traffic congestion and in-flight delays.

NATA and Commuter Air Technology concur with the FAA proposal to
allow part 135 certificate holders to continue to operate with existing
airport requirements, but are concerned about the airport expansion
program. NATA prefers that no new airport legislation be adopted and
that the proposed regulatory allowance for noncertificated airports be
made permanent.

A comment from Fairchild Aircraft mentions the Essential Air
Service Program enacted by Congress that guarantees air service to
small and medium size communities. Fairchild says that the commuter
industry responded to that program and provided essential air service
to small and medium communities, and that those communities may not be
able to afford the proposed airport expansion program.

Other commenters state that it would not be feasible to upgrade
smaller airports to part 139 standards. One certificate holder states
that of the five airports it serves only one meets part 139 standards;
at the other airports where the certificate holder provides essential
air service "there is no aircraft rescue or fire fighting equipment,
airport guidance signs, airfield inspection procedures, airport staff,
snow and ice control plan, or airfield pavement maintenance. . . ."

The American Association of Airport Executives (AAAE), RAA,
Airports Council International-North America, and the National
Association of State Aviation Officials would like the airport
expansion issue referred to an ARAC committee before seeking federal
legislation, to allow ARAC to develop a cost-effective response to NTSB
recommendations that takes into account the difference between small
airports that serve rural communities and large airports near major
cities.

ALPA believes that the FAA should require commuters to operate out
of part 139 certificated airports in the interest of one level of
safety. ALPA recognizes that some airports in remote sites will not be
capable of complying with all part 139 requirements. However, ALPA does
not believe that an exemption should be provided for aircraft with
passenger-seating capacities of 30 or less. Rather certificate holders
that serve small airports should apply individually for an exemption or
waiver.

Commuter Technology expresses concern that a revised part 139 may
result in the application of airplane operator security regulations
of part 108 and the airport security regulations of part 107
to air carriers using aircraft with a seating
capacity of 30 or fewer seats. The commenter believes that the ARAC
committee that is tasked with recommending revisions to part 139 should
also be tasked with restricting or eliminating the applicability of
part 107 to small airports. According to the commenter the application
of parts 107 and 108 to commuter air carriers and the airports that
serve them could have a radical effect on the economic viability of the
air carriers and airports.

FAA Response: The FAA has assigned a task to the Aviation
Rulemaking Advisory Committee (ARAC) to recommend the requirements in
part 139 that should be applicable to airports covered under any
expanded legislation that would give the FAA authority to certificate
airports serving airplanes with less than 30 passengers. In the
meantime, Sec. 121.590 is adopted as proposed to allow affected
commuters to use noncertificated airports. In making its
recommendations ARAC is to consider accepted industry practices
regarding airport safety, personnel available at these airports, costs
associated with meeting these requirements (e.g. capital, operating,
and maintenance costs), and the types of accidents/incidents that have
occurred at these airports.

In response to the comment on security programs for airports and
operators, no changes to parts 107 and 108 are necessary as a result of
this rule because the requirements of those parts are already tailored
to the size of the airplane.

V.H. Effective Date and Compliance Schedule

The FAA proposed an effective date of 30 days and a general
compliance date of 1 year after publication of the final rule. The FAA
stated in Notice 95-5 that a final rule, if adopted, would be published
by December 31, 1995, and that within 1 year of that date, that is, by
December 31, 1996, all affected certificate holders that have air
carrier certification or operating certificates issued under part 135
at the time of publication would have completed the approval process
and obtained new operations specifications giving them authority to
conduct domestic or flag operations under part 121.

Under the proposal, persons who do not already have air carrier
certificates or operating certificates who submit applications for or
obtain air carrier certificates or operating certificates after 30 days
after the publication date of the final rule would be required to
obtain part 121 operations specifications; however, these new entrants
would meet the same requirements as the affected commuters, i.e.,
delayed dates for retrofit of airplanes with certain types of
equipment.

Proposed Sec. 121.2(c) and Sec. 135.2(c) allow for regular or
accelerated compliance with part 121 requirements. Proposed
Secs. 121.2(g) and 135.2(g) also require an affected certificate holder
to submit to the FAA a transition plan for moving from part 135 to part
121.

Comments: Eleven comments were received on this issue. Several
commenters express a desire for an "incremental" or "phased"
compliance schedule. Two commenters are concerned that the proposed
"turnkey" recertification event is high risk with no early rewards or
benefits.

RAA suggests revising proposed Secs. 121.2(c) and 135.2(c) to
require compliance "not later than" 1 year after final rule
publication rather than the proposed "as of," and adding the word
"complete" before "14 CFR part 121 operations specifications." RAA
also suggests adding a new paragraph to the section that would state
that a certificate holder may be authorized under its transition plan
to comply with portions of part 121 instead of the equivalent portions
of part 135 in advance of being issued complete 14 CFR part 121
operations specifications. Accordingly RAA recommends adding to the
transition plan requirements of paragraph (g) a new subparagraph to
include in the transition plans provisions for interim compliance with
portions of part 121 in advance of obtaining complete 14 CFR 121
operations specifications. Other commenters also request provisions for
complying with portions of part 121 in advance of obtaining part 121
operations specifications.

Other commenters also state concerns about FAA's capacity to
facilitate the transition process on schedule. Two commenters perceive
a shortage of trained inspectors and suggest that the compliance date
be extended if an adequate number of inspectors are not provided by mid
year 1996. GAMA suggests a reevaluation of the implementation schedule
of Sec. 121.2(d)(1), citing a questionable number of aircraft
certification service personnel to support the extensive design
approval activity certain to occur. Another commenter expresses concern
over the necessary type certification activity surrounding
modifications and suggests that 1 year is an unrealistic compliance
deadline given the current FAA Aircraft Certification Office backlog.

RAA is concerned that the population of FAA inspectors qualified to
perform their duties under part 121 will not be able to respond to the
new part 121 air carriers. According to RAA, FAA inspectors must be
trained and qualified to help affected commuters achieve the
transition. RAA recommends a "fill in the blanks manual" to achieve
standardization among FAA regions and districts. If there is an
insufficient number of qualified FAA inspectors, the 1996 compliance
date should be delayed.

ASA proposes a standardized transition program including three
elements: (1) a fill-in-the-blanks manual for transitioning carriers;
(2) an automatic exemption and incremental approval process; and (3)
time schedules from transitioning carriers submitted to FAA.

Mesa Airlines recommends pre-formal certification meetings with
principal operations inspectors (POI's) at an early date to familiarize
both parties with the certification process outlined in FAA Order
8400.10. According to Mesa, compliance statement development,
individual operator transition plans, GOM (general operating manual)
development, and formal certificate application should be scheduled for
the spring of 1996 to allow adequate review by respective POI's.
According to Mesa this would allow certificate holders to be running
their commuter operations under part 121 rules by the summer of 1996.
This in turn would allow for a start-up phase for part 121 dispatch
operations and modifications to the requirements for proving runs as
proposed in Sec. 121.163 and would eliminate the necessity for formal
initial operating experience (IOE).

There were several comments on specific compliance dates. ALPA is
generally pleased with the compliance schedule, but states that the 4-
year compliance date for the installation of pitot heat indication
systems could be shortened to 2 years, given the relative ease of the
modification. Fairchild Aircraft finds fault with the fact that a 2-
year delay is provided for compliance with emergency exit handle
illumination, but no delay is allowed for compliance with
Sec. 121.310(b)(2)(ii), which would require the replacement of exit
signs on new commuter category airplanes. Mesa Airlines suggests that
compliance with part 121 crew flight and duty limitations be changed to
January 1, 1997.

FAA Response: The final rule has a 30-day effective date and a
general compliance date of 15 months after publication of the final
rule. The FAA is extending the general compliance date to be
consistent with the compliance date in the training
rulemaking referenced in Section III. E, Related FAA Action. Also, the
proposed delayed compliance dates for certain retrofit requirements
have been modified in response to comments. The final rule also
establishes delayed compliance dates for meeting the performance
operating limitations of part 121 for certain airplanes. Compliance
dates are provided in Sec. 121.2. This section has been reorganized to
separate compliance dates for 10-19 seat airplanes and those for 20-30
seat airplanes. Retrofit and performance requirements compliance dates
are listed on Table 1 and discussed in the appropriate place in the
preamble.

Because of the scope and significance of this rulemaking, the FAA
has already begun planning for the implementation of the final rule.
Training has been provided for inspectors who will be responsible for
overseeing the transition of the affected commuters from part 135 to
part 121 operations. Additional training planned for January 1996 will
focus on the recertification and transition process. Extensive guidance
material is being prepared to assist the inspectors during the
transition process. Portions of this material will also be made
available to the affected commuters.

The FAA agrees with Mesa Airlines that meetings between POI's and
affected commuters would help facilitate the preparation of the
transition plan, which is due 90 days from today, and the planning
necessary to ensure that normal operations can continue during the
transition phase. The FAA believes that the training given to its
inspectors, the guidance material being prepared, and a cooperative
working relationship between the affected commuters and the FAA will
ensure a smooth transition to part 121 operations.

The transition plan must include the certificate holder's proposed
calendar of events that shows how and when it plans to make changes in
its operations to meet the requirements of part 121. The transition
plan should also show detailed plans for accomplishing activities and
necessary retrofits for requirements with delayed compliance dates. The
POI and the certificate holder will schedule the inspections necessary
to show compliance with part 121 requirements. When the inspections are
complete and the FAA has determined that the certificate holder can
comply with part 121, the FAA will issue new operations specifications.
Until the new operations specifications are issued, the existing
operations specifications remain in effect. In any case the existing
operations specifications expire on: (1) The date the new operations
specifications are issued; or (2) 15 months from this date of
publication, whichever is earlier. Affected certificate holders who
want to comply with certain part 121 requirements in advance of being
issued complete 14 CFR part 121 operations specifications could include
in their transition plan a phased schedule including advance compliance
for certain part 121 requirements, subject to their POI's approval.

Table 1--Summary of Modifications shows the compliance dates for
certain retrofit and performance requirements for affected commuters.
Many of these are required by the end of the basic 15-month compliance
period. Affected commuters should be aware that by the specified date
they must comply with all part 121 requirements, not just the ones
listed on Table 1. Although the table includes additional items that
were not listed in the table in Notice 95-5, no new requirements are
involved. Not all requirements are in the table. The purpose of the
table is to show the compliance dates for certain equipment and
performance requirements that necessitate advance planning for
purchasing and installation. Many of the delayed requirements apply to
airplanes in the current fleet, while others apply only to newly
manufactured airplanes.

It should also be noted that Sec. 121.2(h) requires a certificate
holder to comply with corresponding part 135 requirements, as
applicable, in the interval between the effective date of this rule and
when the certificate holder is in compliance with the part 121
requirements. In addition, the intent of Sec. 121.2(h) is also included
in specific sections that have delayed compliance dates.

This table does not apply to certificate holders currently
operating under part 121. The passenger seating configuration numbers
provided in the chart do not mean that the requirement applies only to
that size airplane but rather that the requirement is new for that size
airplane.

Table 1.--Summary of New Equipment and Performance
Modifications for Affected Commuters

Modifications for Affected Communters
-------------------------------------------------------------------------------------
-----------------------------------------
Effective date of required upgrade is as Upgrade will apply to all
airplanes Upgrade will apply to all
stated, measured from the rule including newly
manufactured airplanes newly manufactured
publication date
airplanes
------------------------------------------------------------------------------------
Within ----------------------------
Issue/requirement Within 15 months years (#) After years (#)
----------------------------------------------------------------------------------------------------------------
1. Passenger Seat Cushion Flammability, ........................... 15
10-19 Pax Secs. 121.2, 121.312(c).
2. Lavatory Fire Protection, 10-30 Pax ........................... 2
Secs. 121.2, 121.308.
3. Exterior Emergency Exit Markings, 10- Yes.
19 Pax Sec. 121.310(g).
4. Pitot Heat Indication System, 10-19 ........................... 4
Pax Secs. 121.2, 121.342.
5. Landing Gear Aural Warning, 10-19 Pax ........................... 2
Secs. 121.2, 121.289.
6. Takeoff Warning System, 10-19 Pax ........................... ........... 4.
Secs. 121.2, 121.293.
7. Emergency Exit Handle Illumination, 10- ........................... 2
19 Pax Secs. 121.2, 121.310(e)(2).
8. First Aid Kits, 10-19 Pax Sec. Yes.
121.309(d)(1)(i).
9. Emergency Medical Kits, 20-30 Pax Sec. Yes.
121.309(d)(1)(ii).
10. Wing Ice Light, 10-19 Pax Sec. Yes.
121.341(b).
11. Fasten Seat Belt Light and Placards, Yes \1\ ........... 21.
10-19 Pax Secs. 121.2, 121.317.
12. Third Attitude Indicator, 10-30 Pax:.
Turbojet............................. Yes \2\.
Turboprop Secs. 121.2, 121.305(j)... ........................... 152 15 months.\2\
13. Airborne Weather Radar, 10-19 Pax Yes.
Sec. 121.357.
14. Protective Breathing Equipment, 10-30
Pax.
Sec. 121.2.......................... ........................... 2
Sec. 121.337(b)(8)--Smoke and fume
protection
Sec. 121.337(b)(9)--Fire fighting
(20-30 only)
15. Safety Belts and Shoulder Harnesses, ........................... ........... 15 months.
Single point inertial harness, 10-19 Pax
Secs. 121.2, 121.311(f).
16. Cabin Ozone Concentration, 10-30 Pax Yes.
Sec. 121.578.
17. Retention of Galley Equipment, 10-30 Yes.
Pax Secs. 121.576, 121.577.
18. Ditching approval, 10-30 Pax Secs. Yes \3\.................... 153
121.2, 121.161(b).
19. Flotation means, 10-30 Pax Secs. ........................... 2
121.2, 121.340.
20. Door Key and Locking Door, 20-30 Pax Yes.
Sec. 121.313(f) & (g).
21. Portable O2, 20-30 Pax Sec. 121.327- Yes.
121.335.
22. Additional life rafts, 10-30 Pax Sec. Yes.
121.339.
23. First Aid Oxygen, 20-30 Pax Sec. Yes.
121.333(e)(3).
24. Enroute radio communications, 10-30 Yes.
Pax Sec. 121.99.
25. Latex gloves, 10-30 Pax Sec. Yes.
121.309(d)(2).
26. Passenger information cards, 20-30 Yes.
Pax Sec. 121.571(b).
27. Flashlights-additional for flight Yes.
attendant and pilot, 10-30 Pax Sec.
121.549(b).
28. Flashlight holder for flight Yes.
attendant, 20-30 Pax Sec. 121.310(l).
29. DME, 10-30 Pax Sec. 121.349(c)...... Yes.
30. Single engine cruise performance Yes.
data, 10-30 Pax (required for
determining alternates) Sec. 121.617.
31. Performance, Obstruction Clearance, Yes.\4\.................... 154
and Accelerate-stop Requirements, 10-19
Pax Secs. 121.2, 121.157, 121.173(b),
121.189(c).
----------------------------------------------------------------------------------------------------------------
\1\ In-service airplanes must comply within 15 months. They may use lights or placards. Newly manufactured airplanes must comply with seat belt sign requirements of Sec. 121.317(a) within 2 years.

\2\ Turbojet airplanes must comply within 15 months. Newly manufactured turboprop airplanes must comply within 15 months. In-service 10-30 pax turboprop airplanes must comply within 15 years.

\3\ Transport category must comply within 15 months. Nontransport category can operate for 15 years without ditching approval.
\4\ Commuter category airplanes must comply within 15 months. SFAR 41 and predecessor category airplanes must comply within 15 years.
VI. Discussion of Specific Proposals

In this section specific proposals for part 121 and part 119 are
summarized, comments received are discussed, and the FAA's response to
those comments is given. In Section VII comments received on the costs
and benefits of the proposed rule are addressed. The part 121
discussion, which applies to the affected commuters, appears first
(Section VI.A). Table 2 provides a listing of comparable sections in
part 135 for each specific requirement discussed in this portion of the
preamble. This is followed by a discussion of part 119 issues, which
apply to all certificate holders under part 121 and part 135 (Section
VI.B).
Table 2.--Comparable Sections
in Parts 121 and 135
[This table shows the comparable sections in parts 121 and 135 for each issue discussed in this preamble. Affected commuters, however, must comply with all sections in part 121 that are applicable to their operations, not just the ones listed in this table or discussed in this preamble]
----------------------------------------------------------------------------------------------------------------
Subject 135 Section 121 Section
----------------------------------------------------------------------------------------------------------------
Subparts E and F--Approval of 135.213............................... 121.97, 121.99, 121.101, 121.107.
Routes: Domestic, Flag, and
Supplemental Operations.
Subpart G--Manual Requirements... 135.21, .23........................... 121.133, .135, 121.137.
--Contents and personnel..... ...................................... 121.141.
--Airplane flight manual
Subpart I--Airplane Performance 135.365-.387.......................... 121.175-.197.
Operating Limitations.
Subpart J--Special Airworthiness ...................................... 121.217.
Requirements.
--Internal doors............. 135.87................................ 121.285.
--Cargo carried in the 135 App. A............................ 121.289.
passenger compartment.
--Landing gear aural warning ...................................... 121.291.
device.
--Emergency evacuation and
ditching demonstration.
--New special airworthiness ...................................... 121.293(a) (new).
requirements (retrofit) and
requirements applicable to
future manufactured
airplanes.
--Ditching emergency exits... ...................................... 121.293(b) (new).
--Takeoff warning system
Subpart K--Instrument and
Equipment Requirements:
--Third attitude indicator... 135.149............................... 121.305(j).
--Lavatory fire protection... 135.163 (a), (h)...................... .....................................
--Emergency equipment ...................................... 121.308.
inspection.
--Hand-held fire 135.177(b)............................ 121.309(b).
extinguishers.
--First aid kits and medical 135.155............................... 121.309(c).
kits.
--Crash ax................... 135.177(a)(1)......................... 121.309(d).
--Emergency evacuation 135.177(a)(2), 135.178(c)-(h)......... 121.309(e), 121.310(c)-(h).
lighting and marking
requirements.
--Seatbacks
--Seatbelt and shoulder 135.117............................... 121.311(e), 121.311(f).
harnesses on the flight deck.
--Interior materials and 135.169(a)............................ 121.312(b).
passenger seat cushion
flammability.
--Miscellaneous equipment.... ...................................... 121.313 (c), (f), (g).
--Cockpit and door keys...... ...................................... 121.313(f).
--Cargo and baggage ...................................... 121.587.
compartments.
--Fuel tank access covers.... ...................................... 121.314, .221.
--Passenger information...... ...................................... 121.316.
--Instruments and equipment 135.127............................... 121.317, 121.323.
for operations at night.
--Oxygen requirements
--Portable oxygen for flight 135.157............................... 121.237-.335, 121.333(d).
attendants.
--Protective breathing ...................................... 121.337.
equipment (PBE).
--Additional life rafts for 135.167............................... 121.339.
extended underwater
operations.
--Flotation devices
--Pitot heat indication ...................................... 121.340.
system.
--Radio equipment............ 135.158............................... 121.342.
--Emergency equipment for 135.177, .178......................... 121.353.
operations over uninhabited
terrain.
--TCAS
--Flight data recorders...... 135.180............................... 121.356.
--Airborne weather radar..... 135.152 (a), (b)...................... 121.343.
--Cockpit voice recorders.... 135.173, .175......................... 121.357.
--Low-altitude windshear 135.151............................... 121.359.
systems.
--Ground proximity warning 135.153............................... .....................................
system (GPWS).
Subpart L--Maintenance,
Preventive Maintenance, and
Alterations:
--Applicability.............. 135.411(a)(2)......................... 121.361.
--Responsibility for 135.413............................... 121.363.
Airworthiness.
--Maintenance, preventive 135.423, .425......................... 121.365, .367.
maintenance, and alteration
organization.
--Manual requirements........ 135.427............................... 121.369.
--Required inspection 135.429............................... 121.371.
personnel.
--Continuing analysis and 135.431............................... 121.373.
surveillance.
--Maintenance and preventive 135.433............................... 121.375.
maintenance training
programs.
--Maintenance and preventive ...................................... 121.377.
maintenance personnel duty
time limitations.
--Certificate requirements... 135.435............................... 121.378.
--Authority to perform and 135.437............................... 121.379.
approve maintenance,
preventive maintenance, and
alterations.
--Maintenance recording 135.439(a)(2)......................... 121.380(a)(2).
requirements.
--Transfer of maintenance 135.441............................... 121.380a.
records.
Subpart M--Airman and Crewmember
Requirements:
--Flight attendant complement 135.107............................... 121.391.
--Flight attendants being 135.128(a)............................ 121.391(d).
seated during movement on
the surface.
--Flight attendants or other ...................................... 121.391(e), 121.417, 121.393 (new).
qualified personnel at the
gate.
Subparts N and O--Training ...................................... 121.400-121.459.
Program and Crewmember
Requirements.
Subpart P--Aircraft Dispatcher ...................................... 121.461-121.467.
Qualifications and Duty Time
Limitations: Domestic and Flag.
Air Carriers
Subparts Q, R, and S--Flight Time 135.261-135.273....................... 121.470-121.525.
Limitations and Rest
Requirements: Domestic, Flag,
and Supplemental Operations.
Subpart T--Flight Operations:
--Operational control........ 135.77, .79, 135.75, 135.69, .19...... 121.533, .535, 121.537, 121.547,
121.551, .553.
--Admission to the flight ...................................... 121.557, .559, 121.565 (new).
deck.
--Emergency procedures....... 135.117, .127......................... 121.571(a), 121.533, .573, 121.585.
--Passenger information...... 135.91(d)............................. 121.574.
--Oxygen for medical use by 135.121, 135.87, .122................. 121.575, 121.577.
passengers.
--Alcoholic beverages........ ...................................... 121.578(b).
--Retention of items of mass. 135.93................................ 121.579.
--Cabin ozone concentration.. ...................................... .....................................
--Minimum altitudes for use 135.75, 135.23(q)..................... 121.581, 121.586.
of autopilot.
--Forward observer's seat
--Authority to refuse 135.87, 135.229, .217................. 121.589, 121.590.
transportation.
--Carry-on baggage........... ...................................... 121.617(a).
--Airports
Subpart U--Dispatching and Flight
Release Rules:
--Flight release authority... ...................................... 121.597.
--Dispatch or flight release 135.211............................... 121.611.
under VFR.
--Operations in icing 135.227, .341, 135.345................ 121.629.
conditions.
--Fuel reserves.............. 135.209, .223......................... 121.639, .641, 121.643, .645.
Subpart V--Records and Reports... 135.65(c), 135.415(a)................. 121.701(a), 121.703 (a), (e).
--Maintenance log: Airplane.. 135.417............................... 121.705(b).
--Mechanical interruption 135.439(a)(2), 135.443................ 121.707, 121.709.
summary report.
--Alteration and repair ...................................... .....................................
reports.
--Airworthiness release or ...................................... 121.711, .713, 121.715.
airplane log entry.
--Other recordkeeping
requirements.
----------------------------------------------------------------------------------------------------------------

VI.A. Part 121 Discussion

VI.A.1. Subpart E--Approval of Routes: Domestic and Flag Air Carriers

Section 121.97 requires each domestic and flag operator to show
that each route it submits for approval has enough airports that are
properly equipped and adequate for the proposed operation. The operator
must also have an approved system to disseminate this information to
appropriate personnel. Although part 135 has similar requirements, part
121 requires more information.

Section 121.99 requires each domestic and flag operator to have a
two-way air/ground communication system between each airplane and the
appropriate air traffic control facility, along the entire route. In
the 48 contiguous States and the District of Columbia, the
communications system between each airplane and the dispatch center
must be independent of any system operated by the United States. This
would be a new requirement for the affected certificate holders.

Section 121.101 requires each domestic and flag operator to show
that enough weather reporting facilities are available along each route
to ensure weather reports and forecasts necessary for the operation.
For operations within the 48 contiguous States and the District of
Columbia, these reports must be prepared by the National Weather
Service. For other areas, a system must be approved by the
Administrator. Section 135.213 has similar requirements, except that
the pilot in command is allowed to use various other sources, including
his own weather assessment, for VFR operations. This section also
requires reports of adverse weather phenomena. The FAA proposed that
affected certificate holders comply with part 121.

Section 121.107 requires each domestic and flag operator to have
enough dispatch centers, adequate for the intended operation. This
would be a new requirement for affected certificate holders, as
discussed in Section V.F., Dispatch System.

Comments: ALPA comments that the upgrade to part 121 represents a
major improvement over part 135. ALPA also comments that Subparts E and
F should be upgraded to require that each pilot have a set of approach
and navigation charts rather than having to share a set. ALPA provides
supportive information, such as an NTSB recommendation (A-95-35) for a
similar requirement.

Several comments were received on the enroute radio communication
requirements of Sec. 121.99. ASA and RAA question the need for airline
provided enroute radio communication capability for short-haul flights
and request that the requirement be reconsidered. According to these
commenters, the average enroute times for affected certificate holders
is less than an hour. For such short flights there is little time
during the enroute portion of a flight for company communication. The
cost of installing company communications would be high and safety
would not be diminished without company communication since the crew
can be contacted through Air Traffic Control.

AACA points out that this would be a new requirement for affected
commuters. Intrastate Alaskan operations now conducted under flag
operations rules will be conducted under domestic rules and would be
required to comply with the independent communications systems
requirements. Because of low altitudes, VFR flight operations, and the
lack of Remote Communications Outlet at many locations, maintaining
communications will require construction of a large communications
infrastructure. When operators in Alaska use flag rules, AACA
interprets Sec. 121.99 to not require the communications system be
independent of any system operated by the United States.

FAA Response: The ALPA suggestion on requiring that each pilot have
a separate set of navigation and approach charts is beyond the scope of
this rulemaking; however, the FAA is planning to initiate a separate
rulemaking on the issue.

Section 121.99 requires each domestic and flag air carrier to have
a two-way radio communication system that is independent of any system
operated by the United States. FAA flight service stations and air
traffic control facilities that are currently providing radio
communication service for certificate holders are used for the control
of aircraft and were never intended to be used by individual
certificate holders to relay information that is the certificate
holder's responsibility, such as scheduling changes or weather
information. Hence, an additional expense would be incurred by
certificate holders required to contract for communication services
through commercial services. However, it is believed that most part 135
certificate holders already have facilities and communications
equipment that satisfy the dispatch requirements under part 121.

The FAA believes that there is a need for a two-way air-ground
radio communication system that will ensure reliable and rapid
communications over the entire route between each airplane and the
appropriate dispatch office and between each airplane and the
appropriate air traffic control unit. The need to show that each
operator has a two-way radio system is not new. However, the
requirement to have an independent system is new for operations of
affected commuters and intrastate Alaska and Hawaii operations
previously conducted under flag operations rules. While no commenters
focus on Sec. 121.97 or Sec. 121.117, the FAA points out under
Secs. 121.97(b)(4)(i) and 121.117(b)(4)(i) affected
operators will be required to comply with airport data requirements
which include applicable performance requirements of Subpart I. For
affected airplanes these performance requirements will be found in new
appendix K to part 121 as referenced in subpart I.

VI.A.2. Subpart F--Approval of Routes: Approval of Areas and Routes for
Supplemental Air Carriers and Commercial Operators

This subpart is similar to subpart E except that it applies to
supplemental operations and prescribes flight following requirements.
Under the proposal, this subpart would apply in cases where an affected
operator uses an airplane that is also used in domestic operations to
conduct a nonscheduled operation. On this issue, no comments were
received and the final rule is adopted as proposed.

VI.A.3. Subpart G--Manual Requirements

Manual requirements: Contents and personnel: Under subpart G of
part 121 certificate holders are required to prepare and keep current a
manual containing policies, procedures, applicable regulations, and
other information necessary to allow crewmembers and ground personnel
to conduct the operations properly (see Sec. 121.133 and Sec. 121.135).
While the requirements of parts 121 and 135 are similar, part 121
manual requirements contain a more extensive list of manual contents
(Sec. 121.135). Under part 121 the manual or appropriate parts must
also be furnished to more personnel, such as aircraft dispatchers and
flight attendants, and made available to others, such as station
agents. Notice 95-5 stated that the effect of these differences between
compliance with part 121 versus compliance with part 135 would be
significant for commuter operators. The proposal would require
developing, producing, and distributing new manuals appropriate to part
121. In addition, Sec. 121.137 requires the air carrier to issue a
manual or appropriate parts to each crewmember and requires each
crewmember to keep the manual up to date and have it with him or her
when performing assigned duties. Part 135 does not require that flight
attendants be issued a manual; however, it does require that any person
to whom a manual is issued must keep it up-to-date (see Sec. 135.21).

Comments: Fairchild Aircraft states that Sec. 121.137 would require
at least one copy of the manual specified by Sec. 121.133 to be carried
in the airplane and that this is a reasonable proposal that they fully
support. Fairchild Aircraft also states that Sec. 121.141(b)(2)
contains a reference to "rotorcraft" which should be deleted.

ALPA states that the key to an efficient, safe airline operation
can normally be found in the manuals developed by the airline. ALPA
supports the FAA in adopting all facets of Subpart G. ALPA also states
that Sec. 121.135(b)(2) should be amended by removing, "in the case of
supplemental air carriers and commercial operators," so that the
paragraph reads: "Duties . . . of the ground organization, and
management personnel." According to ALPA, the requirement to include
in the manual duties and responsibilities of management personnel would
no longer be applicable only to supplemental and commercial operators
since proposed part 119 requires management personnel for all
certificate holders.

One commenter states that Sec. 121.133 should require compliance
with the certificate holder's manuals.

Metro International Airways states that the cost of new manuals
would be excessive for small businesses and that an outline of
procedures would be a more useful reference than a highly detailed
manual.

FAA Response: All but one of the comments received regarding the
manual requirements support the implementation of Subpart G of part
121. Only one comment regarding the costs associated with the manuals
required by Sec. 121.131 was received.

Additionally, the FAA has received requests from certificate
holders that would like to begin the process of transition prior to
implementation of the rule. This would allow those certificate holders
to spread the cost of manual production and distribution over a longer
period of time. The question of phased-in-implementation is not unique
to this issue and is addressed elsewhere in this document.

The FAA agrees with ALPA's suggestion to revise the wording of
Sec. 121.135(b)(2). This is not a substantive change from Notice 95-5
because Sec. 119.65(e) also requires that manuals contain the duties
and responsibilities of required management personnel. The FAA also
agrees with Fairchild's suggestion to delete the word "rotorcraft"
from Sec. 121.141(b)(2). These recommendations are appropriate. In the
final rule Secs. 121.135(b)(2) and 121.141(b)(2) are revised
accordingly.

In response to the comment that Sec. 121.133 should require
compliance with the certificate holder's manual, the holder of an air
carrier certificate with operations specifications to operate under
part 121 must comply with the regulations in part 121 (and other
applicable regulations). Requirements for preparing and maintaining a
manual serve the purpose of supplying information to personnel.
Information in the manual must be accurate and consistent with the
regulations. Since the manual may also include company policy and
guidance to personnel, all portions of the manual are not enforceable
as regulations. The language of the manual requirements does, however,
imply that the certificate holder must adhere to all of the contents of
the manual and that the certificate holder's personnel must use the
manual in conducting operations.

In response to the comment that the manual requirements will be a
burden for small businesses and that an outline of procedures would be
more helpful to personnel, small certificate holders are already
meeting the manual requirements of part 135; this rulemaking requires
an update of manuals and broader distribution of the manuals. An
outline of procedures could be used as guidance in addition to the
manuals or as part of a manual, but under current part 135 it would not
suffice as meeting the manual requirements.

In the final rule Sec. 121.133 has been revised to update the
terminology.

VI.A.4. Subpart H--Airplane Requirements

For comments and FAA responses to the requirements in Sec. 121.157,
Aircraft certification and equipment requirements, see the discussion
in Section V. C., Aircraft Certification.

Single-engine airplanes. Section 121.159 prohibits operation of
single-engine airplanes under part 121. No change to this prohibition
was proposed since the FAA does not consider single-engine airplanes
acceptable to part 121 standards. Under the proposal, this section was
amended to delete an obsolete reference to Sec. 121.9. No comments were
received on this issue and the final rule is adopted as proposed. For a
related discussion on the operation of single-engine Otters, see
"Applicability: Alaska," in Section V.B.

Airplane limitations: Type of route. Section 121.161(a) requires
that a two-engine or three-engine airplane except a three-engine
turbine powered airplane must be within 1-hour flying time from an
adequate airport at normal cruising speed with one engine inoperative,
unless otherwise approved by the Administrator. Part 135 does not
contain a comparable requirement; however, the FAA proposed that
affected commuters would comply with the requirements of
Sec. 121.161(a).

Section 121.161(b) contains a separate requirement that (with some
exceptions for certain older airplanes) no person may operate a land
plane in extended overwater operations unless it is certificated or
approved as adequate for ditching. The FAA proposed that affected
commuters would also comply with the requirements of Sec. 121.161(b).
In Notice 95-5, the FAA invited specific comments on the potential
impact of these proposals on operations in Alaska.

Comments: Several comments were received on the Sec. 121.161(a)
requirement to be within 1 hour of an airport with one engine
inoperative. One commenter suggests that Sec. 121.161 be rewritten to
reflect today's environment, since no airport in the U.S. is more than
1 hour away for these commuter airplanes. The commenter also states
that the rule should specify the requirements for two-engine operations
over the water.

Fairchild and AIA both state that Sec. 121.161(a) would require
single-engine cruising speed data and this data is unlikely to be
included in some Airplane Flight Manuals (AFM). The commenters also
state that there appears to be no safety benefit and it will be
difficult to show compliance. According to these commenters, the final
rule should except 10-30 passenger seat airplanes.

Phoenix Air anticipates that its operations with a Grumman G-159
Gulfstream airplane would be disrupted due to the requirements of
Sec. 121.161, since they intend to start service between Honolulu and
Midway Island. There are no airports that would be within 1 hour of the
intended flight path.

Jetstream concurs with the requirement that airplane routes should
be within 1 hour of an adequate airport.

Three comments were received on the certification ditching
requirements of Sec. 121.161(b). Fairchild and AIA note an apparent
oversight in that the FAA did not propose to exclude part 23 Normal or
Commuter Category airplanes from the ditching requirements of
Sec. 121.161(b).

AACA notes that several certificate holders fly affected aircraft
on extended overwater routes in Alaska. Compliance with the part 25
ditching requirements would add certification costs, impose equipment
weight penalties, and reduce payloads. According to the commenter, the
FAA did not calculate these costs. The commenter supplies information
indicating that costs to comply with the ditching requirements of part
25 are substantial.

FAA Response: Despite the comments to the contrary, the FAA has
decided to adopt its proposal to apply the route limitation
requirements of Sec. 121.161(a) to the 10- to 30-seat airplanes
operated by the affected commuters. Under that section any route flown
by a twin engine commuter type airplane must be flown so that it is
within 1 hour of an adequate airport for landing. Part 121 and its
predecessor regulations have applied route limitation requirements to
airplanes operating under those requirements since 1936. While the
specific details of the route limitation requirement have changed over
the years, the underlying safety issue has not; the certificate holder
must show, before operating affected airplanes over a route, that it
can safely continue flight in an emergency situation to an airport
adequate for landing. The FAA understands that some of these airplanes
will require an AFM revision that will provide engine-out cruise speed
data. There are routes in areas outside of the contiguous U.S. that are
more than 1 hour flying time (with one engine inoperative) from an
adequate airport. In accordance with Sec. 121.161(a), the Administrator
may authorize a deviation from the requirement, if the operator can
show that the 1-hour flight time limit is not necessary based on the
character of the terrain, the kind of operation, or the performance of
the airplane. Obtaining authorization to conduct extended range
operations with two-engine airplanes is dependent upon many factors.
Some of these factors are a type design review of the airframe system,
a review of the in-service history of the airplane propulsion system,
and an assessment of the certificate holder's maintenance and
inspection program capability for extended range operations. Advisory
Circular 120-42 provides the guidelines for this authority. Other rules
provide the requirements for extended overwater routes.

The Douglas DC-3 and Curtiss C-46 airplanes excluded from
Sec. 121.161(b) were type certificated and manufactured before the
present standards of part 25 were adopted. These aircraft were excluded
because of their previous operating experience which showed, in some
cases through actual ditchings, that these old airplanes could ditch
satisfactorily. The Convair 240, 340, and 440 and Martin 404 airplanes
were also type certificated before the present standards were adopted.
They were excluded because tests conducted by the National Advisory
Committee for Aviation showed they would have excellent ditching
characteristics. Unlike current part 25, part 23 contains no standards
for ditching approval. Unlike those older airplanes excluded in
Sec. 121.161, none of the part 23 airplanes have been shown to comply
with any ditching standards. Contrary to the commenter's assumption,
requiring part 23 airplanes used in extended overwater operations to
meet the ditching certification requirements was not an oversight. In
Notice 95-5 preamble, the FAA concluded that these requirements should
be applied to the operations that would be moved from part 135 to part
121.

After considering the comments, the FAA has determined that until
15 years after the date of publication of the final rule a certificate
holder may operate in an extended overwater operation a nontransport
category land airplane type certificated after December 31, 1964, that
was not certificated for ditching under the ditching provisions of part
25 of this chapter. Section 121.161(c) has been added accordingly.

Proving tests. Section 121.163 provides proving test requirements
for part 121. In addition to aircraft certification tests, an aircraft
to be operated under part 121 must have at least 100 hours of proving
tests for an airplane not previously proven for use in part 121
operations, and 50 hours of proving tests for an airplane previously
proven for use in part 121 operations. The number of hours may be
reduced by the Administrator. Section 135.145 requires 25 hours of
proving tests in addition to certification tests for certificate
holders that operate turbojet airplanes or airplanes for which two
pilots are required for operations under VFR if that airplane or an
airplane of the same make and similar design has not been previously
proved in any operations under part 135. Both Secs. 135.145 and 121.163
require proving tests for materially altered airplanes. However, under
Sec. 121.163, proving tests apply to each airplane to be operated under
part 121. Under part 135 proving tests apply to each aircraft or to
aircraft of similar make and design. Part 121 also describes three
types of proving tests. Under part 121, the initial operator of a type
of airplane must conduct at least 100 hours of proving tests,
acceptable to the FAA, which can be reduced in appropriate
circumstances. Moreover, for each kind of operation (e.g., domestic,
flag, supplemental) that a certificate holder conducts, 50 hours of
proving tests are required, which are reducible in appropriate
circumstances.

Comments: Six substantive comments were received. Comair and RAA
concur with the requirement for an air carrier to demonstrate
its ability to perform in accordance with part 121 and
company procedures. However, Comair proposes that carriers currently
conducting operations under part 121 and part 135 (split certificates)
should not be required to conduct this demonstration. Carriers
conducting part 121 and part 135 operations have previously proven
their ability to conduct part 121 operations. If the requirement for
dispatching is adopted, flight crewmembers will demonstrate their
proficiency with the new system during their required line check.

RAA comments that proving flight hours should be reduced based on
"experience and performance" factors. To facilitate a reduction in
flight hours, the FAA should identify those specific procedures for
which non-revenue proving flights would be required and specify a
realistic number of flights or flight hours which would be sufficient
to demonstrate those procedures.

ASA believes that the requirement for proving flights will result
in an increase in both initial and recurring costs. United Express
joins ASA in proposing that FAA recognize the experience level of air
carriers operating under part 135 and permit proving tests to be
conducted during revenue service. United Express further proposes that
the required number of hours be reduced for those carriers currently
using a dispatch system.

Big Sky Airlines recommends a waiver of the requirement for a
proving test for airlines that have a good safety record and proven
experience. The commenter justifies its recommendation on the basis of
excessive and unnecessary burden and cost.

Commuter Air Technology requests clarification concerning which
modifications to specific aircraft would require 100-hour initial
proving tests.

FAA Response: Section 121.163 has two main parts. Paragraph (a)
prohibits a carrier from operating an aircraft type in scheduled
service that has never been used in scheduled service until it has
flown 100 hours of proving flights. These hours are in addition to any
aircraft certification tests. For the purposes of this rulemaking, the
FAA recognizes that the current commuter fleet has established a
sufficient history of operations and does not intend to require the 100
hours of proving flights for aircraft currently being operated by those
carriers affected by this rulemaking. Paragraph (b) of Sec. 121.163
requires 50 hours of tests for the carrier to show that not only can it
operate and maintain the aircraft, but also that it has the ability to
conduct a particular kind of operation (i.e., domestic or flag) in
compliance with the applicable regulatory standards.

The FAA agrees that carriers currently conducting operations under
both part 121 and part 135 (split certificates) will be eligible to
apply for a reduction of the number of hours required to conduct the
demonstration required by paragraph (b). In regard to the comment that
flight crewmembers that are new to part 121 operations will demonstrate
their proficiency during accomplishment of a line check, the FAA does
not agree that this could take the place of proving flights. The
primary focus of proving flights is not simply to test the proficiency
of flight crewmembers but to test the company's operational control
procedures for the airplanes that will be operated in accordance with
the requirements for a new kind of operation, i.e., flag or domestic.
The FAA supports the idea that proving flight hours should be reduced
based on "experience and performance" factors. The FAA has begun to
identify those specific procedures for which proving flights would be
required and to specify a realistic number of flights or flight hours
which would be sufficient to demonstrate those procedures. This
guidance to FAA inspectors will be provided in a revision to Order
8400.10.

The FAA agrees that proving tests will require an expenditure of
the carrier's financial resources. Safety requires these proving tests
to determine that an operator can conduct operations under part 121
safely, using new procedures, dispatches, etc. The FAA recognizes the
experience level of air carriers operating under part 135 and, based on
the carrier's experience with part 121, will provide FSDO inspectors
with written guidance on approving deviations from the requirements of
Sec. 121.163. The FAA believes that proving tests are an essential part
of the certification process and also provide the carrier with an
opportunity to do some "dry-runs" before beginning revenue service
under a completely new set of regulatory standards. The FAA's intent is
to provide inspectors with the authority to provide deviations from the
proving test requirements. FAA Headquarters will review each proposed
reduction of proving test hours and will concur or not concur with the
proposed number of hours for each affected commuter.

In response to Commuter Air Technology's request for clarification
concerning which modifications to specific aircraft would require 100
hour initial proving tests, Sec. 121.163(d) contains criteria for when
a type of aircraft is considered to be materially altered in design.

VI.A.5. Subpart I--Airplane Performance Operating Limitations.

Subpart I contains airplane performance operating limitations that
apply to all part 121 certificate holders; however, not every section
in subpart I applies to every certificate holder. For example,
Secs. 121.175 through 121.187 apply to reciprocating engine-powered
transport category airplanes and Secs. 121.189 through 121.197 apply to
turbine engine-powered transport category airplanes (with an exception
for certain reciprocating-powered airplanes that have been converted to
turbo-propeller-powered). Sections 121.199 through 121.205 apply to
nontransport category airplanes.

In part 121 the term "nontransport category airplane" is
currently used to refer to older airplanes like the Curtis C-46, that
were type certificated before the transport category was established,
i.e., the early 1940's. However, many airplanes type certificated over
the last 20 years used by affected commuters (e.g., commuter category
and SFAR 41 airplanes and predecessor categories), are also
nontransport category. Therefore, the FAA proposed to delete the term
"transport category" throughout subpart I and to include language
where appropriate to except airplanes type certificated before January
1, 1965, that were not certificated in the transport category. This
would have the effect of requiring airplanes type certificated in the
commuter category or a commuter category predecessor to be operated
under the performance operating limitations of Secs. 121.175 through
121.197, as applicable.

Comments: ALPA states that all requirements of part 121 subpart I
should be complied with by all turbo-propeller airplanes with a
passenger capacity of 10 or more.

AACA concurs that airplanes with 10 to 19 seats should be required
to comply with all of the proposed modifications (in Table 1 of Notice
95-5) except for part 121 performance and obstruction clearance and
floor proximity lighting. (See later discussion of floor proximity
lighting.)

Jetstream, RAA and ALPA support the overall proposals concerning
the higher level of performance requirements. However, they join with
Commuter Air Technology, Raytheon and an individual to point out that
additional performance data/charts would need to be developed (for
example: accelerate-stop and obstacle clearance data). RAA also
recommends a 2-year time frame instead of the proposed 1-year
performance compliance date.

Jetstream states that Notice 95-5, in conjunction with other
proposed rules and changes, will introduce more weight to the aircraft.
In addition to this, AC 120-27D, Aircraft Weight and Balance Control,
will increase standard average passenger weights used for calculations.
The combined effect is that these aircraft will no longer be allowed to
carry 19 passengers due to reduced payload capacity. According to the
commenter, the combined effect of the weight changes is about two
passengers.

Jetstream and Raytheon comment that current FAA policy should be
revised to allow manufacturers to increase the maximum takeoff weights
for aircraft certificated under SFAR 41. They justify their comments by
stating that the increase in maximum takeoff weight will provide a
mitigation of the additional equipment weights incurred under this
rulemaking.

One commenter states that better weight and balance control by the
FAA is necessary because many operators are flying over maximum weight.

Fairchild, Jetstream, and AIA propose that the FAA incorporate the
language of Sec. 135.181(a)(2) into Sec. 121.191, which would provide,
in their view, a more conservative approach to one engine inoperative
enroute operations. Jetstream also notes that there is no requirement
for commuter airplanes to show Net En Route Flight Path data in their
AFM's.

One commenter suggests that part 121 be written to specify the
exact performance requirements for nontransport category airplanes to
be included in their performance manuals so there would be no confusion
with other FAA performance requirements.

Fairchild and AIA suggest deleting all references to "transport
category" in Secs. 121.189 through 121.197.

FAA Response: Section 121.135(b) requires that the manual contain
methods and procedures for maintaining the aircraft weight and center
of gravity within approved limits. Approved weight and balance control
procedures are the only means for an operator/applicant to authorize
the use of other than known weights for crew, passengers, baggage, or
cargo. The weight and balance control program, including loading
schedules and charts, are approved on operations specifications by the
FAA. This program must be included in the operator/applicant's policies
and procedures manual.

Section 121.189(c)(1) states, for turbine engine powered takeoff
limitations, that "(c) No person operating a turbine engine powered
category airplane certificated after August 29, 1959, may take off that
airplane at a weight greater than that listed in the Airplane Flight
Manual (AFM) at which compliance with the following may be shown: (1)
The accelerate-stop distance must not exceed the length of the runway
plus the length of any stopway."

The FAA agrees that new or additional performance data would need
to be developed for certain airplanes, and that this data would need to
be acceptable to the FAA Aircraft Certification Office and incorporated
into the Airplane Flight Manual (AFM). At the present time, some AFM's
(for Beech 99, certain Metroliners, and the Twin Otter) do not have
accelerate-stop distance data, only accelerate-slow data. In order for
the airplane operator to comply with Sec. 121.189(c)(1), the operators
would have to request an AFM supplement from the airplane manufacturers
showing this required data. The FAA has not required the manufacturers
to develop this data. If they have developed the data, it would still
have to be certificated by the FAA as a revision to the AFM. If the
manufacturer does not have accelerate-stop data, it will have to flight
test, simulate, or analytically prove accelerate-stop distance data to
the FAA. This process could be expensive to the operators who would pay
for the manufacturer's support.

This rulemaking does not require the affected airplanes that are
currently in service or airplanes that will be manufactured under an
existing type certificate to meet the engine-out climb gradient
performance required by part 25. These airplanes will, however, be
required to meet the obstacle clearance limitations of
Sec. 121.189(d)(2).

Section 121.189(d)(2) states for turbine engine powered takeoff
limitations, that "(d) No person operating a turbine engine powered
category airplane may take off that airplane at a weight greater than
that listed in the Airplane Flight Manual--(2) In the case of an
airplane certificated after September 30, 1958, that allows a net
takeoff flight path that clears all obstacles either by a height of at
least 35 feet vertically, or by at least 200 feet horizontally within
the airport boundaries and by at least 300 feet horizontally after
passing the boundaries." AFM's for some older airplanes with seating
capacity of 10-to-19 passengers do not have data to show the required
climb gradient or the certification basis to clear obstacles after
takeoff with an engine-out at a specified weight. As one commenter
suggests, additional certification requirements would have to be
identified in part 121 or in a new Appendix to 121 for nontransport
category airplanes, except for the commuter category or SFAR 41, ICAO
Annex 8 airplanes, before these airplanes could comply with
Sec. 121.189(d)(2) requirements.

As with accelerate-stop data, the FAA agrees that new or additional
performance obstacle clearance data for certain airplanes would need to
be developed, and that this data would need to be approved by an FAA
Aircraft Certification Office and incorporated into the Aircraft Flight
Manual. Raytheon estimates that to provide obstacle clearance data,
testing would have to be done on all Beech 99 models and the price per
each airplane for the new performance data would be $63,000 ($53,000
for the Beech 1300). This cost must be incurred by the manufacturer and
then passed on to all the operators.

The FAA recognizes the significant problems in developing the
necessary performance data for airplanes type certificated under a wide
range of standards over the past 30 years, including part 23 (or its
predecessor, part 3 of the Civil Air Regulations) normal category, plus
additional standards in the form of special conditions, SFAR 23, SFAR
41C, or part 135, appendix A, or part 23 commuter category. Development
of the additional performance data for airplanes certificated under
older standards may be developed by conducting actual flight tests,
data analysis, or any other methods acceptable to the Aircraft
Certification Office. The FAA believes that the performance
requirements of Sec. 121.189(d)(2), obstacle clearance with an engine-
out after takeoff, contribute to an increased level of passenger and
crew safety.

The FAA also understands that the requirements for accelerate-stop
and obstruction clearance may, in fact, remove certain airplanes from
service in part 121. It may also affect the operational capability of
some operators, depending on the location and height of obstacles, and
may terminate air carrier service to some communities if airplanes are
removed from service.

Because of the difficulty that affected commuters would face in
meeting the part 121 performance operating limitations with their
existing fleet, the FAA has decided to provide delayed compliance for
these requirements. Subpart I has been amended to state different
requirements for aircraft used by affected commuters that were
certificated under different certification standards, as follows:

1. Airplanes certificated under commuter category can meet all of
the airplane performance requirements of part 121 within 15 months of the
publication of the final rule.

2. Airplanes certificated under SFAR 41 or earlier certification
standards will be allowed to continue to comply with the part 135
Subpart I and other airplane performance operating limitations
requirements for 15 years. The FAA anticipates that some of the SFAR 41
airplanes will be able to meet the part 121 requirements within the 15-
year period so they have the choice of either continuing to operate
under the performance requirements of part 135 for the 15-year
compliance period or complying with the performance requirements of
part 121 during the 15-year compliance period. Some of the airplanes
certificated under earlier certification standards, such as under part
135, Appendix A, part 23, with special conditions, and SFAR's 23 and
41C, will probably never be able to meet the part 121 standards. For
affected commuters operating these airplanes, the 15-year period allows
the operators sufficient time to plan for and obtain replacement
airplanes or to modify them.

Although the FAA encourages affected commuters to comply with the
performance operating requirements earlier than 15 years after
publication of the final rule, it is allowing that length of time to
ensure that there will be an adequate supply of replacement airplanes
available for purchase. The current rate of production of new commuter
category airplanes is approximately 30 per year. But most importantly,
if the FAA were to impose a shorter compliance period and affected
commuters were not able to obtain new airplanes from manufacturers,
they might replace their equipment with airplanes configured for fewer
than 10 passengers. This airplane group is not covered by this
rulemaking and has a higher accident rate than the 10-19 passenger
airplanes. Therefore, an unintended effect of this rule could be an
increase in the accident rate.

In response to Jet Stream's comment, current FAA policy prohibits
revisions to airplanes certificated under SFAR 41 that would increase
the maximum weight or the number of passengers. This SFAR was
terminated on September 13, 1983.

While the FAA understands that some of the older airplanes (i.e.,
normal category predecessors of commuter category airplanes) may not be
able to meet certain performance requirements, the FAA has determined
that some performance requirements, such as the maintaining of an
altitude with an engine-out, are important safety enhancements that
provide for a higher level of safety. This level of safety required in
part 121 should be available to all passengers flown on carriers
operating under part 121.

Section 121.191 requires that the AFM show a one-engine inoperative
net en route flight path which would provide a positive slope at an
altitude of at least 1,000 feet above the terrain (2,000 feet in
mountainous terrain) within 5 statute miles of the intended track.
Section 121.191 also provides for a net flight path that would allow
continued flight from the cruising altitude to an airport clearing all
terrain and obstructions. Section 135.181(a)(2) requires airplanes to
maintain a 50 feet per minute rate of climb when operating at the MEAs
or 5,000 feet MSL whichever is higher. It does not provide for the
continuation of the flight below the MEA.

Section 121.191 has continuously provided for safe engine out en
route operations while allowing some flexibility. The flexibility
allows the certificate holder to calculate maximum weights for
maintaining a constant engine out altitude, a continuous flight path
drift down to an airport when an altitude cannot be maintained, and
provides off airways direct routing engine out performance
requirements. The FAA understands that net en route flight path data
must be provided by the manufacturer; however, the FAA believes that
part 121 air carriers deserve the additional flexibility of
Sec. 121.191 and that commuters adopting the Sec. 121.191 requirements
may gain a flexible benefit with a continued higher level of safety.

In response to comments, the FAA points out that Notice 95-5
proposed to remove the words "transport category" wherever they
appear in subpart I.

In reviewing part 121 to resolve comments, the FAA noted that
several formulas are printed incorrectly. In the rate of climb formula
for reciprocating engine powered transport category airplanes
certificated under parts other than part 4a of the Civil Air
Regulations (CAR), the parentheses are misplaced. This formula has been
printed correctly in the corresponding part 135 section of Sec. 135.371
(a) and (c)(1). Also, in the rate-of-climb formula for transport
category airplanes certificated under CAR 4a [Sec. 121.181 (a) and
(c)(1) and Sec. 121.183 (a)(2) and (c)(1)] it is not clear as printed
that the subscript <INF>So is to be squared. Appropriate corrections
are made to both formulas.

VI.A.6 Subpart J--Special Airworthiness Requirements

Internal doors. Section 121.217 prescribes that in any case where
internal doors are equipped with louvers or other ventilating means,
there must be a means convenient to the crew for closing the flow of
air through the door when necessary.

Comments: Raytheon Aircraft states that a new toilet installation
for the 1900D has internal partitions with permanently open louvers.
Compliance with Sec. 121.217 would require Raytheon to redesign the
partition louvers so a crewmember could leave his or her station to
close the louvers when necessary or design the louvers for remote
control closure.

FAA Response: Contrary to the commenter's assumption, the lavatory
partition louvers in the commenter's airplanes would not have to be
redesigned. As stated in Sec. 121.213 (a) and (b), Sec. 121.217 applies
only to airplanes type certificated under Aero Bulletin 7A or part 04
of the Civil Air Regulations.

Cargo carried in the passenger compartment. Section 121.285
requires that cargo carried in passenger compartments must be stowed in
a fully enclosed bin or carried aft of a bulkhead or divider and
properly restrained. Section 135.87 allows certificate holders to carry
cargo in an approved cargo compartment instead of a fully enclosed bin
and to carry restrained cargo anywhere in the passenger compartment if
it is restrained by a net that meets the requirements of
Sec. 23.787(e). The FAA proposed to amend Sec. 121.285 to add an
exception for commuter category (and predecessor) airplanes that would
have the effect of allowing cargo to be carried in the passenger
compartment as it is today under part 135.

Comments: AACA, an association of Alaskan air carriers, fully
supports the proposal.

FAA Response: The final rule includes provisions from Sec. 135.87
that have been moved into Sec. 121.285 for nontransport category
airplanes type certificated after December 31, 1964.

Landing gear aural warning device. Section 121.289 contains a
requirement for a landing gear aural warning device for large
airplanes. At present this section applies to any airplane with a
maximum certificated takeoff weight of more than 12,500 pounds.
Appendix A of part 135 requires a landing gear warning device for
airplanes having retractable landing gear and wing flaps, but the
device need not be aural. The FAA considers that the cost of replacing
a warning light with a warning sound would be minimal. Therefore,
this section would apply to any airplane
that presently operates under part 135 and that would be required by
this final rule to operate under part 121. To allow adequate time for
airplanes without aural warning devices to be retrofitted, the FAA
proposed a compliance date of 2 years after the publication date of the
final rule.

Comments: Raytheon comments that their models all provide aural
landing gear warning.

AACA notes that the FAA did not prepare a cost analysis for this
proposal, other than to show that the cost would be "minimal." AACA
shows that various manufacturers' comments on similar proposals have
identified substantial administrative, engineering, installation, and
ongoing maintenance cost. However, AACA also notes that, in this case,
Fairchild Aircraft believes that the landing gear aural warning can be
installed without undue cost or difficulty.

AACA also states that once an item is installed, there are many
other things that must be done that involve cost. Cost items identified
are: revisions of the certificate holder's training program, normal and
emergency procedures, maintenance MEL's and other items need to be
amended to reflect the change from a visible lighted warning device to
an aural device. According to AACA, compliance costs add up
incrementally to substantial cumulative cost and that the FAA fails to
account for.

FAA Response: Even though part 23 requires an "aural or equally
effective device," the FAA is not aware of airplanes where the
"equally effective device" was accepted as the only warning for the
landing gear warning. The reason for not accepting such devices
includes the consideration of pilot's work load during the landing
phase of flight and the need for the warning to attract pilot attention
under such conditions. No proposed lighted device, by itself, has been
found acceptable to provide the needed warning for this flight
condition. Therefore, the FAA is amending Sec. 121.289 as proposed to
require installation of a landing gear aural warning device within 2
years of the publication of this final rule. However, the FAA believes
that all affected airplanes already have an aural warning system.

Emergency evacuation and ditching demonstrations. Section 121.291
contains requirements for conducting demonstrations of airplane
evacuation and ditching procedures. The FAA requires these
demonstrations upon introduction of a new type and model of airplane
into passenger-carrying operations. For airplanes with a seating
capacity of more than 44 passengers, an actual evacuation demonstration
must show that the full capacity of the airplane and the crewmembers
can be evacuated within 90 seconds. Also, for airplanes with more than
44 passenger seats a partial demonstration is required under one of the
circumstances described in Sec. 121.291(b). Demonstrations have not
been required for airplanes with fewer than 44 passenger seats.

Under Sec. 121.291(d) any certificate holder operating or proposing
to operate one or more landplanes of any size in extended overwater
operations must conduct a simulated ditching in accordance with
Appendix D to part 121. The purpose of the ditching demonstration is to
show that the certificate holder's ditching training and procedures for
a new type and model of airplane are satisfactory. The simulated
ditching does not specifically require the use of flight attendants;
the FAA proposed to apply this rule to any affected commuter operator
who conducts extended overwater operations, whether or not flight
attendants are used in the operation. The FAA proposed to apply this
provision to the affected commuter operators only when a new type and
model of airplane is introduced into the certificate holder's
operations after the effective date of the final rule. This requirement
does not apply to the current fleet.

The FAA proposed to amend Sec. 121.291(b) to clarify that the
partial demonstration procedures apply only to airplanes with more than
44 passenger seats.

Comments: With respect to partial evacuation, one commenter states
that the proposed rule would reduce the safety requirements for
commuters because the evacuation procedures under part 121 do not apply
to airplanes with less than 44 seats and that Sec. 23.803 requires a
demonstration for commuter category airplanes. One commenter states
that Sec. 121.291(b) does not indicate if the requirement applies to
aircraft with more than 44 seats or all aircraft.

Two commenters recommend clarifying the rule language for the
ditching demonstration in Sec. 121.291(d) to make the FAA's intent
clear. The commenters say that the current language does not properly
communicate the fact that a ditching demonstration would be required
only if an airplane is a new make/model for a particular certificate
holder's fleet.

FAA Response: Parts 25 and 121 currently require emergency
evacuation demonstrations for transport category airplanes with more
than 44 passenger seats. These demonstrations are required in addition
to specific detail design requirements, e.g. aisle width, exit size,
exit slides, etc., and are conducted to confirm the overall evacuation
capability of the airplane. They are also conducted to show the
adequacy of the operator's evacuation procedures. Considering the
specific detail design requirements with which transport category
airplanes must also comply, the FAA has not found it necessary to
require such evacuation demonstrations for airplanes having 44 or fewer
passenger seats. Since part 135 does not pertain to operations with
airplanes having more than 44 passenger seats, there has been no need
to require an emergency evacuation demonstration in that part. Part 23,
on the other hand, does not contain the same specific detail design
requirements for commuter or predecessor normal category airplanes.
Therefore, an evacuation demonstration is required for type
certification of those airplanes in lieu of the specific detail design
requirements that transport category airplanes must meet. There will be
no reduction in safety because transport category airplanes will still
be required to comply with the same specific detail design requirements
and the part 23 requirement for an evacuation demonstration will remain
unchanged. As proposed, Sec. 121.291(b) is amended to make clear that
it, as well as Sec. 121.291(a), only applies to airplanes with more
than 44 passenger seats.

The FAA agrees that the language in Sec. 121.291(d) for the
ditching requirement does not clearly state that it applies to the
affected commuters only if an airplane is a new type and model
introduced after they began operations under part 121. Therefore,
clarifying language is added to Sec. 121.291(d).

New special airworthiness requirements (retrofit) and requirements
applicable to future manufactured airplanes:

-- Ditching emergency exits. Section 25.807(e) contains
requirements for ditching emergency exits in transport category
airplanes. The ditching exits for transport category airplanes with 10
or more passenger seats must meet at least the dimensions of a Type III
passenger emergency exit (20 inches wide by 36 inches high). It should
be noted that transport category airplanes are required to have
ditching exits meeting those criteria regardless of whether the
airplane is approved for ditching and used in extended
overwater operations. If ditching approval is requested
by the applicant, it also must be shown that the
required life rafts can be launched successfully through the ditching
emergency exits.

Part 23, as recently amended by Amendment 23-46 (59 FR 25772; May
17, 1994), now contains requirements for ditching exits; however, all
of the normal or commuter category airplanes currently in service were
type certificated before that amendment became effective. The FAA
proposed to amend part 121 (proposed new Sec. 121.293(a)) to require
ditching exits for nontransport category airplanes type certificated
after December 31, 1964. Unlike those required for transport category
airplanes, the ditching exits would only have to be as large as those
currently required by Sec. 23.807(b) (19 inch by 26 inch ellipses). The
FAA proposed that compliance would be required 2 years after the
publication date of the final rule. The proposed requirement would not
entail adding new exits. The overwing exits of most airplanes type
certificated under part 23 would probably qualify as ditching exits.
Part 25 airplanes intended for non-part 121 transportation sometimes
comply by providing a sheet metal dam that can be installed in the
passenger entry doorway. If it is necessary to consider a floor-level
exit as a ditching exit in a nontransport category airplane, a similar
sheet metal dam could be provided.

Comments: Commuter Air Technology, a modifier of business airplanes
for commuter airline service, states that its product has overwing
exits that would be usable anytime the airplane was floating. The
commenter questions whether it would be necessary to conduct a $5,000
type certification effort to qualify those exits as ditching emergency
exits. NATA, an association representing certificate holders of 10- to
19-passenger-seat airplanes, recommends rescinding the proposal and
asserts that the cost of compliance would be extremely high. The
commenter offers no specific details concerning costs, but does note
that de Havilland DHC-6 Twin Otters have experienced only three
ditchings in 17 million flight hours.

FAA Response: The comments received have some validity. The
majority of the current commuter fleet, at least those for which
ditching exits were not substantiated for certification, includes such
airplanes as the Beechcraft 99 and 1900 and Fairchild airplanes with
low wings and overwing exits. It is likely that these exits would
qualify as ditching emergency exits. However, they would have to be
tested. That would also be true of all other low-wing part 23 normal or
commuter category airplanes that would be operated under part 121.

In addition to the low-wing models, there are also three high-wing
normal or commuter category airplane models. These are de Havilland
DHC-6, Twin Otters, which are by far the most numerous of the high-wing
models, and the Dornier 228 and Britten Norman BN-2A Mk III
Trislanders. (This, of course, refers to landplanes. Many Twin Otters
operate as seaplanes on floats.) Typically, high-wing landplanes come
to rest in the water on the fuselage with one wing tip in the water.

The DHC-6 Series 100 and 200 airplanes have emergency exits in the
top of the fuselage forward of the wing. These exits also meet the
ditching emergency exit requirements. The DHC-6 Series 300 airplanes do
not have such overhead exits; instead they depend entirely on the
emergency exits in the sides of the fuselage. In almost three decades
of service with Twin Otters, there have been two ditchings. One
involving a Series 100 airplane occurred in the Pacific Ocean during a
ferry flight from Long Beach, California, to Honolulu, Hawaii. Another,
involving a Series 300, occurred in the Arctic. In both instances, all
occupants were evacuated safely. In the latter case, the occupants
escaped through the exits on the highest side. The FAA is not aware of
any ditchings of Trislanders or Dornier 228 airplanes; however, because
the Dornier 228 and the Trislander are so similar in design to the DHC-
6, it is likely that they would float the same way that the Series 300
airplane did, and that their exits would also meet the ditching
emergency exit requirements.

Most of the part 23 commuter and predecessor normal category
airplanes are low-wing airplanes with overwing exits that would comply
with no further substantiation required. The vast majority of the
airplanes would, therefore, not be affected by the requirement in
regard to either cost or safety benefit because they already comply. In
view of the successful ditchings that have occurred with high wing
airplanes to date, the FAA has decided not to adopt Sec. 121.293(a) as
proposed.

-- Takeoff warning system. Section 25.703 requires an aural
warning to the flightcrew at the beginning of the takeoff roll when the
wing flaps, leading edge devices, wing spoilers, speed brakes, and
longitudinal trim devices are not in a position that would allow a safe
takeoff. Part 23 does not require a takeoff warning system (although a
requirement for such a system is proposed in Notice No. 94-21, 59 FR
37620, July 22, 1994); in addition, part 23 airplanes typically do not
have multiple types of devices. Accidents have occurred on transport
category airplanes when the flightcrews initiated takeoffs when the
airplanes were not in the proper configurations for takeoff. The FAA
proposed that airplanes manufactured after a date 4 years after the
publication date of the final rule would be required to have a takeoff
warning system as required by Sec. 25.703. However, a warning system is
not required for any device for which it can be demonstrated that
takeoff with that device in the most adverse position would not create
a hazardous condition (Sec. 121.293(b)).

Comments: One commenter notes that a takeoff warning would not be
required under Sec. 25.703 if it is demonstrated that a takeoff with
that device in the most adverse position would not create a hazardous
condition. This commenter questions how one can measure the effect of
these improper settings when compounded by other unfavorable
conditions, such as weight and balance mistakes, but does not express
support or opposition to the proposal.

Commuter Air Technology discusses the longitudinal trim and flap
systems on its airplanes. The commenter notes that the pilot can
visually verify that the flaps are in correct 40 deg. takeoff setting
from the cockpit. The commenter also states that the longitudinal trim
is manual and has center marking visible from both the pilot and co-
pilot positions. The commenter's position is that the additional cost
of such a system is not warranted.

FAA Response: The first commenter correctly notes that a takeoff
warning system is not required for any devices if it is demonstrated
that takeoffs with that device in the most adverse position would not
cause an unsafe condition. While the FAA agrees that with some
airplanes it is possible to verify visually flap positions and manual
trims and that there is a cost to install warnings, the FAA has
determined that for safety reasons, an aural warning is needed under
the conditions described.

In considering these comments, the FAA notes that all of the in-
service airplanes have demonstrated, by their service histories, that
there is no device position that would cause an unsafe condition and
therefore that there would be no need for installation of additional
takeoff warning devices. While proposed Sec. 121.293(b) (now
Sec. 121.293) does not apply to any in-service airplanes affected by
this rule, the requirement for airplanes manufactured 4 years
after the publication date of this rule is
retained in the final rule to ensure that future airplanes are covered.

VI.A.7. Subpart K--Instrument and Equipment Requirements.

Instrument and equipment requirements are contained in part 121,
subpart K, and part 135, subpart C. The requirements are in addition to
the airplane and equipment requirements of part 91. The discussion
below emphasizes all new or revised equipment requirements except for
major equipment such as FDR's and airborne weather radar, which are
previously discussed in the "Major Issues" section of this document.

Notice 95-5 proposed to require that commuter operators comply with
part 121 airplane and equipment requirements except in areas that were
specifically discussed.

Sections 121.303, 121.305, and 121.307 require certain airplane
instruments and equipment. Some of the part 121 equipment is required
under part 135 only for IFR, VFR over-the-top, and VFR night
operations. Most of the airplanes used by affected commuters already
have these instruments as well as equipment required under part 135
(Secs. 135.143 and 135.149). Under the proposal this equipment in these
part 121 sections would be required for all part 121 operations.

Third Attitude Indicators. Section 121.305(j) currently requires a
third attitude indicator on large turbojet-powered and large turboprop
powered airplanes. Notice 95-5 proposed to apply this requirement to
airplanes that would be operating under part 121 as a result of this
rulemaking.

Comments: Most of the commenters on this issue oppose the
requirement, primarily because of the cost.

According to RAA, part 121 does not include an equivalent to
Sec. 135.163(h), which requires dual attitude indicators which are
powered by two different and independent power sources for nontransport
category airplanes. RAA recommends requiring the third attitude
indicator only for new production large airplanes, deleting the
proposed retrofit requirement, and incorporating Sec. 135.163(h) into
part 121 for nontransport category airplanes. RAA also recommends
considering an equivalent means of compliance for large nontransport
category airplanes, such as "Situation Awareness for Safety" devices.

Raytheon Aircraft and Mesa state that the requirement is excessive
for airplanes that already have two attitude indicators, each supplied
by a separate source of power. Raytheon and Big Sky are concerned that
the requirement might necessitate a redesign of the instrument panel.

Twin Otter International believes the requirement would be
extremely costly with little safety benefit. According to Twin Otter,
even if the attitude indicator were lost, the airplane would have
adequate performance and information to be operated without a third
attitude indicator.

Commuter Air Technology concurs with the proposal for all aircraft
operated under part 121 and points out that Sec. 135.149 currently
requires a third indicator only for turbojet aircraft.

United Express states that the FAA supporting data for a third
(independently powered) attitude gyro is based on turbojet accident/
incident research and not on turbopropeller accident/incident data.
According to the commenter, until the FAA can substantiate that this
will prevent accident recurrence in turbopropeller aircraft, it should
not be required. The commenter states that some aircraft, such as the
commenter's fleet of Jetstream turboprops, have a third attitude gyro
powered by the aircraft battery system. No information has been
provided, that the commenter is aware of, suggesting that an
independent power source will improve safety or accident statistics in
turbopropeller aircraft.

FAA Response: Section 121.305(j) currently requires a third
attitude indicator on large turbojet-powered and large turboprop-
powered airplanes. Part 135 requires a third attitude indicator only
for turbojet powered airplanes.

The FAA's intent as stated in Notice 95-5 was to require all
affected airplanes to comply with the equipment requirements of
Sec. 121.305 including the requirement for a third attitude indicator.
The notice did not contain amendatory language to Sec. 121.305(j);
however, to be consistent with the FAA's stated intent, the rule
language has been developed to include the intended airplanes and to
provide a compliance date.

In response to RAA's comment that part 121 does not have an
equivalent to Sec. 135.163(h), which requires two independent sources
of energy, each of which is able to drive all gyroscopic instruments,
such an equivalent appears in Sec. 121.313(e).

The FAA does not agree with the commenter that a third attitude
indicator is excessive for airplanes that have two attitude indicators
or that there could be little safety benefit. The final rule requires a
third attitude indicator in all turbojet powered airplanes and all
turbopropeller powered airplanes. However, the FAA recognizes that
retrofit installation of a third attitude indicator imposes a burden
which may require a redesign of the instrument panel. Therefore, as
with certain other requirements, the final rule provides for a 15-year
compliance date for turbopropeller powered airplanes having a passenger
seating configuration of 10 to 30 seats that were manufactured before
15 months after the date of publication of this final rule. In effect,
this allows operators to decide whether to retrofit these airplanes or
phase them out. Turbojet airplanes and newly manufactured turboprop
airplanes must comply within 15 months.

Lavatory fire protection. Section 121.308 currently requires
lavatory smoke detection systems, or equivalent, and automatically
discharging fire extinguishers in lavatory receptacles for towels,
paper, or waste for passenger-carrying transport category airplanes.
The FAA proposed to apply the requirements of Sec. 121.308 to airplanes
formerly operated under part 135 that are equipped with lavatories.
Section 121.308 would be amended to delete the references to transport
category. The proposed compliance section, Sec. 121.2, required that
lavatory protection equipment be installed within 2 years after the
publication date of the final rule.

Comments: ALPA believes that the FAA should require installation of
the smoke detection system within 6 months of the effective date rather
than 1 year as proposed. This commenter also believes that installation
of the lavatory fire suppression system should be required in all
airplanes newly manufactured within 1 year of the effective date rather
than 2 years as proposed.

ASA and RAA do not object to compliance insofar as new airplanes
are concerned, but do suggest that the requirement be deleted as a
retrofit requirement. These two commenters state that the industry
estimated cost of compliance is $2,500 per airplane while Jetstream
estimates $4,000 per airplane.

Comair believes compliance would amount to $2,500 and 20 pounds per
airplane. The commenter asserts that compliance is not justified for
airplanes with 20 to 30 passenger seats due to the small size of the
cabin, proximity of a trained flight attendant with a portable fire
extinguisher, and the present smoking ban on domestic flights.

Commuter Air Technology asks whether the proposed requirement would
apply to some of their products that have a side facing
toilet separated from the cabin only by a
curtain.

Jetstream states that there is no evidence to support the
introduction of fire suppression of toilet receptacles on commuter
aircraft. According to the commenter, the lavatory receptacles are
already designed to contain a fire within the compartment; and, due to
the small cabin size of those airplanes, the lavatory is readily
accessible to the crew if the need to suppress a fire does occur. The
commenter estimates a cost of $4,000 per airplane. Nevertheless, the
commenter does support requiring new aircraft to comply.

FAA Response: The FAA does not agree with the commenter's
suggestion that installation of smoke detectors should be done within 6
months and fire extinguishers within 1 year of the publication of the
final rule. This would not allow sufficient time for compliance.

The comments received do not contradict the FAA's understanding
that few, if any, of the airplanes with 10 to 19 passenger seats are
equipped with lavatories. The primary impact of the proposed
requirement for lavatory smoke detection and fire extinguishment,
therefore, would be on airplanes with 20 to 30 passenger seats
presently operated under part 135. (Any such airplanes currently
operated under part 121 are already required to comply.)

Contrary to one commenter's belief, the present smoking ban on
domestic flights does not eliminate the need for lavatory smoke
detection and fire extinguishment. On the contrary, the smoking ban
could increase the temptation for some passengers to smoke illicitly in
the lavatory and thereby increase the possibility of a fire originating
in that compartment. The presence of a smoke detector serves as a
deterrent to illicit smoking as well as a means of warning when it does
occur.

Contrary to the commenter's belief, the presence of a flight
attendant in the cabin would not compensate for the lack of a lavatory
smoke detector and fire extinguisher. A lavatory is designed with an
effective ventilation system to preclude normal odors from entering the
cabin. In the absence of a smoke detector, the ventilation systems also
precludes early detection of illicit smoking or a fire by persons in
the cabin. In addition, the materials typically contained in the waste
receptacles are highly flammable and could burn out of control quickly
if there were no automatically discharging extinguishers. It is
possible that a flight attendant would not know the fire exists until
it has grown to catastrophic proportions.

The cost estimates provided by two commenters appear to be based on
a misunderstanding concerning the qualifications of a required lavatory
smoke detector. Such detectors serve primarily to enhance the
capability of crewmembers to detect lavatory fires visually. They are,
therefore, not required to meet all of the performance and
environmental requirements applicable to primary detectors used in
isolated compartments, such as cargo compartments. Anything that meets
the ordinary dictionary definition of a lavatory would be covered by
this requirement.

Therefore, because the adverse service experience that prompted the
adoption of Sec. 121.308 applies equally to any airplane, large or
small, with a lavatory and because the commenters' cost estimates are
obviously based on a misunderstanding of the required smoke detector
qualification, the FAA is adopting this requirement in substance as
proposed. The final rule has been revised to provide operators 2 years
from the date of publication to comply with the lavatory smoke detector
system and fire extinguisher requirements. In addition, the rule states
that operators of 10- to 19-seat airplanes that have a lavatory must
have a smoke detector system or equivalent that provides either a
warning light in the cockpit or an audio warning that can be readily
heard by the flightcrew. This will accommodate airplanes that do not
have flight attendants.

Emergency equipment inspection. Section 121.309(b) requires that
each item of emergency and flotation equipment must be inspected
regularly in accordance with inspection periods established in the
operations specifications to ensure its condition for continued
serviceability and immediate readiness to perform its intended
emergency purpose. Section 135.177(b) contains a similar requirement
for part 135 operators of airplanes with more than 19 seats. In this
section, the FAA proposed requiring affected commuter operations,
including those with airplanes of 10 to 19 seats, to comply with the
existing part 121 requirement. Other provisions in the proposal would
require affected commuters to install additional emergency equipment.
No comments were received on this issue and the final rule is adopted
as proposed.

Hand-held fire extinguishers. Sections 121.309(c) and 135.155
contain similar requirements for hand-held fire extinguishers aboard
airplanes. Part 121 requires at least two of the fire extinguishers to
contain Halon, or an equivalent, and mandates placement of the fire
extinguishers, while part 135 does not. In Notice 95-5, the FAA
proposed that affected commuters comply with the part 121 requirements
for fire extinguishers and that Sec. 121.309(c)(7) be amended to
require that at least one of the fire extinguishers in the passenger
compartment contain Halon or the equivalent. No comments were received
on this issue and the final rule is adopted as proposed.

First aid kits and medical kits. Section 121.309(d) requires that
both approved first aid kits and approved emergency medical kits be
carried on board passenger-carrying airplanes. The medical kits are
intended to be used only by medically qualified persons, such as
doctors, who may be on board the airplane. Section 135.177(a)(1)
requires first aid kits to be carried on board airplanes with more than
19 passengers.

The FAA proposed that first aid kits be required for all airplanes
with more than 9 passenger seats operating under part 121 and medical
kits be required for airplanes that are required to have a flight
attendant. The FAA stated in Notice 95-5 that, after review of the
comments, the FAA might decide to require a medical kit for all 10-19
seat airplanes.

In Notice 95-5 the FAA pointed out that affected commuters would
have to comply with a recent rule requiring disposable latex gloves for
first aid kits and medical kits.

Comments: Six commenters disagree with the proposed requirement to
have first aid kits on 10- to 19-seat airplanes. Most of the commenters
cite lack of space and the lack of necessity for the equipment.
Commenters believe that the first aid kit would not provide enough of a
medical benefit to justify its cost. Two of these commenters oppose the
addition of latex gloves as part of the first aid kit. One commenter
believes that the equipment would place additional liability on
employees. One commenter concurs with both proposed requirements.

Two commenters provide additional cost information for first aid
kits. One of the commenters estimates $1,500 per airplane and the other
estimates $1,500 without specifying the number of entities involved
(i.e., airplane(s) or fleet).

AACA agrees with the requirement for first aid kits on all commuter
airplanes whether a flight attendant is available or not. According to
the commenter, regardless of the size of the airplane, inflight
emergencies could occur and a first aid kit may be needed. In the
absence of a flight attendant, a crewmember or passenger could use the
first aid kit. The commenter also estimates costs of $4,359 for Alaskan
commuter air carriers in the first year and $436 each year thereafter
to meet the requirement, but there is no explanation of the detail.

Four commenters disagree with the required medical kits on 20 to 30
seat airplanes. These commenters cite lack of space and the lack of
necessity for the equipment. Three commenters argue that medical kits
should not be required on airplanes with less than 30 seats due to the
lack of trained personnel and the low likelihood that a medical
professional would be on board. One commenter believes that the
equipment would place additional liability on employees. One commenter
concurs with the proposed requirements.

One commenter provides a cost estimate of about $2,000 per airplane
for the medical kit requirement. However, the cost estimate is not
supported by any documentation.

FAA Response: The FAA maintains that certain of these requirements
are necessary to enhance safety. The ability to respond in the early
stages of a medical emergency is critical and could save lives in the
event of an in-flight injury or an accident. Additionally, the FAA
maintains that latex gloves as were required by a 1994 rule change (59
FR 55208, November 4, 1994) should be included in these first aid kits
because they guard against transmission of disease through spilled
blood. In sum, no commenter provides any compelling reason to eliminate
the first aid kit requirement, especially considering that these
airplanes often operate in remote areas where medical assistance may
not be available. The FAA has determined that emergency medical kits
will be required for airplanes requiring a flight attendant. For
airplanes not having a flight attendant, requiring a medical kit poses
problems, such as a lack of security, no one to monitor the use of the
kit, and no one to check the credentials of a person who professes to
be a doctor and able to administer the medical treatment.

The regulations allow flexibility in the location and mounting
methods of kits. Depending on the weight of the kit and Velcro surface
area, Velcro may be sufficient. Even if Velcro is not practical in a
particular instance, other low-cost alternatives, such as leather
straps with buckles, are acceptable.

Crash ax. Section 121.309(e) requires that each airplane be
equipped with a crash ax, while Sec. 135.177 requires a crash ax for
airplanes with a passenger seating configuration of more than 19
passengers. Under part 135 the crash ax is to be accessible to the crew
but inaccessible to the passengers during normal operations. The FAA
proposed in Sec. 121.309(e) to require a crash ax for each airplane
that has a flight deck separate from the passenger cabin and a lockable
door.

Comments: One commenter disagrees with the FAA assertion in Notice
95-5 that the crash ax is useful only for egress from the flight deck
to the cabin in the event of an emergency. The commenter says that the
Airplane Flight Manual of one popular 19-seat commuter airplane
suggests that preparation for certain gear-up landings include opening
an overwing exit inflight, because even relatively minor distortion of
the fuselage in a small airplane can render exits unusable. Thus, the
crash ax could be used for prying open an exit.

Raytheon states that if a key lock is required as proposed on
lockable doors in 10- to 19-seat airplanes, then a crash ax would be
required. The commenter states that removal of the door would eliminate
the requirements for a lock and a crash ax.

A third commenter supports the proposal as written in Notice 95-5
to require a crash ax only in airplanes that have a separate flight
deck with a lockable door.

FAA Response: The primary purpose in requiring that a crash ax be
carried is to allow emergency egress after an accident if airplane
exits are unuseable. However, the FAA agrees with commenters that there
could be other uses for the ax including egress of the cockpit crew.

After considering the comments and reviewing the proposed
requirement, the FAA has determined not to require crash axes on
nontransport category airplanes type certificated after December 31,
1964, primarily because these airplanes are not required to have a
lockable door. The FAA has determined that the lockable doors that
exist in nontransport category airplanes type certificated after
December 31, 1964, are frangible and obviate the need for a crash ax on
the flight deck. Also carrying a crash ax in these airplanes creates a
security risk since the ax would not be inaccessible to passengers.

Emergency evacuation lighting and marking requirements. Section
121.310(c), by referencing Sec. 25.812(e), requires emergency
evacuation lighting for passengers when all sources of illumination
more than 4 feet above the floor are totally obscured. This requirement
applies to all transport category airplanes regardless of how many
passenger seats they have. There is no corresponding requirement in
part 23 or in part 135 for airplanes having a passenger-seating
configuration of less than 20 seats.

Section 121.310(d) for emergency light operation requires that each
light required by paragraphs (c) and (h) must be operable manually and
must operate automatically from the independent lighting system. As
proposed, these requirements would apply to affected commuters. In
Sec. 121.310(d)(2)(i) each light must be operable manually both from
the flightcrew station and from a point in the passenger compartment
that is readily accessible to a normal flight attendant seat.

Section 121.310(e) requires that an exit operating handle may not
be used if its brightness decreases below a specified level. Section
135.178(e) contains an identical requirement for airplanes having a
passenger seating configuration of more than 19 seats. Under the
proposal the requirement would also apply to airplanes with a passenger
configuration of 10-19 seats.

Section 121.310(f) contains standards for access to various exit
types that presently apply only to transport category airplanes.
Section 135.178(f) is identical to Sec. 121.310(f) for airplanes having
a passenger configuration of more than 19 seats. The FAA proposed to
amend Sec. 121.310(f) to exclude nontransport category airplanes.

Section 121.310(g) (and its parallel requirement in Sec. 135.178(g)
for more than 19 passenger seat airplanes) requires emergency exits to
be marked on the outside by a 2-inch band contrasting in color with the
surrounding fuselage. Most airplanes with a passenger-seating
configuration of less than 20 seats operating under part 135 are
already required to meet this requirement and, for those that do not,
compliance with this requirement as proposed would merely require
painting the bands around each exit.

Section 121.310(h) requires airplanes for which the application for
type certification was made before May 1, 1972, to meet the exterior
emergency lighting standards of Sec. 25.812, in effect on April 30,
1972, or any later standards in effect if the application for type
certification was made later. The FAA proposed to require nontransport
category airplanes type certificated after December 31, 1964, (i.e.,
part 23 normal and utility category) to comply with Sec. 25.812 in
effect April 30, 1972, within 2 years after the publication date of a
final rule.

The FAA proposed that airplanes with a passenger-seating
configuration of less than 20 seats previously operated under part 135
be required to comply with the above-described emergency
lighting systems (that is, emergency exit signs, interior lighting,
exit handles, and exterior lighting) and, except for the marking
requirement discussed above, proposed a compliance date 2 years after
the publication date of a final rule.

Comments: Sixteen comments were received on proposed Sec. 121.310.
All commenters oppose the proposal to retroactively require any
additional emergency exit signs or emergency lighting on 10-to-19
passenger seat commuter airplanes.

Several commenters state that the cost of retrofitting in-service
airplanes with an emergency lighting system would be much more
expensive than the FAA expected when the notice was prepared.

Six commenters note the size of the cabin area of these airplanes
and that no person is seated more than 8 feet (or two or three rows)
from an exit. One of these six also notes that no person is more than
12 feet from two exits.

Four commenters note that an emergency evacuation demonstration is
required for the certification of commuter category airplanes and that
these demonstrations have shown that the airplanes can be evacuated,
under conditions of total darkness, in less than 90 seconds. Two other
commenters note that there is no known service history or adverse
accident data related to commuter operations to support the need for
this proposal. Therefore, all six of these commenters believe there is
no justification for the proposal and each of them recommends that it
be withdrawn.

One commenter believes that the current briefing on exit locations
and their use is sufficient and that no further action is needed. Two
commenters believe that the requirement in Sec. 121.310(c)(3) to show
compliance with Sec. 25.812(e) does not add any safety to these
airplanes. They point out that the height of the ceiling in their
airplane is only 4\3/4\ feet high and question the need to comply with
the provision of Sec. 121.310, which requires compliance with
Sec. 25.812(e). Section 25.812(e) requires escape path markings for
passenger guidance, "when all sources of illumination more than four
feet above the cabin aisle floor are totally obscured." According to
commenters, with a ceiling height of only 4\3/4\ feet, it is likely
that the required exit markings are located less than 4 feet above the
floor and that compliance with Sec. 121.310(c)(3) is not necessary.
Another commenter believes that the requirement in Sec. 25.812 for
emergency lighting to operate for 10 minutes is not needed for these
airplanes. The commenter points out that the required emergency
evacuation time for these airplanes is much less than 10 minutes and
that this requirement should be adjusted accordingly. One other
commenter suggests that flashlights be made available. Finally, two
commenters acknowledge that emergency lighting may enhance safety;
however, they also believe that this enhancement in safety can be
provided by a lighting system that is less expensive, less complex, and
much lighter than the one envisioned by Sec. 121.310. Accordingly, they
provide some suggestions for such a system.

Embraer, a foreign manufacturer of transport category airplanes,
believes that Sec. 121.310(f) should also be amended to exclude smaller
(e.g., 20 to 30 passenger) transport category airplanes as well as
nontransport category airplanes. The commenter believes that a
passenger seat would have to be removed from its product for operation
under part 121 if smaller transport category airplanes were not also
excluded from this section.

AACA supports the proposed amendment to Sec. 121.310(g).

The only other comment received concerning this issue was from an
individual who requests resolution of the issue of whether the 2-inch
wide contrasting band has to be on the fuselage surrounding the
emergency exit or on the exit itself.

FAA Response: Section 23.803 does require an emergency evacuation
demonstration, as noted by the commenters; however, the demonstration
is required primarily to compensate for the differences in evacuation
design features (e.g. aisle width, exit size, etc.) required by part 23
and those of part 25. Like the demonstrations required by part 25 for
airplanes with more than 44 passengers, the demonstrations are intended
to evaluate the evacuation capability of the airplane under standard
conditions and are not intended to show the evacuation capability of
the airplane under the most adverse condition that could be
encountered. They are not intended, for example, to demonstrate the
evacuation capability of the airplane when there is dense smoke in the
cabin or when there is hazardous, damaged structure in the vicinity.
The applicability of the required evacuation demonstrations to the need
for emergency lighting is therefore limited.

Passengers must egress rapidly in the event of fire. Contrary to
the commenters' assertions concerning a lack of adverse service
experience, the FAA is aware of at least six instances since 1980 in
which passengers had to be evacuated because of fire from such
nontransport category airplanes or transport category airplanes with
cabins of similar size. There is no doubt that safety can be enhanced
considerably by requiring compliance with the emergency lighting
requirements proposed in Notice 95-5. Nevertheless, the installation of
such lighting is very costly.

In response to excluding smaller airplanes from the requirements
pertaining to access to exits, Sec. 121.310(f)(2) states, in part, that
there must be enough space next to each Type I or Type II emergency
exit to allow a crewmember to assist in the evacuation of passengers
without reducing the unobstructed width of the passageway below that
required (20 inches wide). Part 135 contains the same requirement for
airplanes having a passenger seating capacity of more than 19 seats.

Since the commenter's product has more than 19 passenger seats and
numerous examples are already in service in this country, the airplanes
have presumably been shown to comply with either Sec. 135.178(f)(2) or
the identical text of Sec. 121.310(f)(2). Thus, this rulemaking would
not impose any new burden on airplanes with more than 19 passenger
seats.

Section 121.310(g) states that exterior exit markings "must be a
2-inch wide colored band outlining each passenger exit on the side of
the fuselage." Since the band is outlining the exit it would be on the
fuselage, not on the exit.

After reviewing the costs and benefits associated with the proposed
emergency lighting requirements, the FAA has decided to revise the
final rule as follows:

1. The floor proximity lighting requirements in Sec. 121.310(c)
will apply to all airplanes except non-transport category airplanes
type certificated after December 31, 1964. In effect, this is not a
change from current requirements. Affected airplanes with 10 to 19
passenger seats will not have to comply because of the small cabin
size, the probability that passengers would be able to find the
emergency exits without floor lighting, and the high cost of
retrofitting for these requirements.

2. The interior light operation requirements of Sec. 121.310(d) do
not apply in the final rule to nontransport category airplanes
certificated after December 31, 1964, since the requirements of
Sec. 121.310 (c) and (h) apply only to transport category airplanes.

3. The requirement for an illuminated exit operating handle
(Sec. 121.310(e)) remains as proposed. The compliance date for retrofit
requirements for 10- to 19-seat airplanes is 2 years after publication
of the final rule.

4. Section 121.310(f) was proposed to apply to airplanes with a
passenger-seating configuration of more than 19 seats. This remains in
the final rule.

5. The requirement for marking emergency exits on the outside in
Sec. 121.310(g) remains as proposed since compliance is relatively
simple and inexpensive for all affected operators.

6. The exterior lighting standards in Sec. 121.310(h) are revised
to except nontransport airplanes type certificated after December 31,
1964.

Seatbacks. Section 121.311(e) prohibits a certificate holder from
taking off or landing unless passenger seats are in the upright
position. Section 135.117 requires only that passengers be briefed that
seats should be in the upright position. The FAA proposed that affected
commuters be required to comply with Sec. 121.311.

Comments: One commenter objects to the requirement because the
pilots cannot assure compliance in a 19-seat airplane, especially
during landing.

FAA Response: The FAA intended for those flights with flight
attendants to be operated in accordance with the current Sec. 121.311.
For these flights on nontransport airplanes type certificated after
December 31, 1964, the FAA has included wording to clarify that the
pilot must only instruct the passengers to place their seatbacks in the
upright position. The final rule has also been revised to add a new
subparagraph to Sec. 121.311(e) that provides that on an airplane with
no flight attendant, the certificate holder may take off or land as
long as the flightcrew instructs each passenger to place his or her
seatback in the upright position. This change is needed to clarify what
is required for airplanes that do not have a flight attendant.

Seat belt and shoulder harnesses on the flight deck. Section
121.311(f) requires a combined seat belt and shoulder harness with a
single-point release that meets the requirements of Sec. 25.785. Part
135 does not contain a requirement for a single-point release system
although the FAA believes that virtually all commuter category
airplanes being manufactured today have such a system. To ensure that
this is the case for newly manufactured airplanes, the FAA proposed in
Sec. 121.2(e)(1) to require that airplanes manufactured after 1 year
after publication of the final rule meet the requirements of
Sec. 121.311(f).

Comments: One commenter concurs with the proposal.

FAA Response: The final rule remains substantively as proposed,
except that compliance is within 15 months after publication of the
final rule. However, to clarify that Sec. 121.311(f) applies to newly
manufactured nontransport category airplanes, appropriate language is
added to that paragraph.

The final rule also revises Sec. 121.311(h) to allow crewmembers
for affected commuters to release the shoulder harness if they cannot
perform their duties otherwise.

Interior materials and passenger seat cushion flammability. Section
25.853(b) was amended in 1984 to require seat cushions to meet greatly
enhanced flammability standards. At the same time, Secs. 121.312(b) and
135.169(a) (but not for commuter category airplanes) were amended to
require airplanes already in service to meet the improved seat cushion
flammability standards after November 1987. In the years that have
passed since that date, the improved cushions are credited with saving
a number of passengers' lives.

The FAA proposed to require nontransport category airplanes type
certificated after December 31, 1964, to comply with the same seat
cushion flammability standards that apply to other airplanes operated
under part 121. The proposed compliance date was 2 years after the
publication date of the final rule or on the first replacement of the
cushions, whichever occurs first. The proposed rule also allowed for
granting deviations for up to 2 additional years when justified by
unique integral-seat cushion configurations.

The FAA also proposed that the interior components of nontransport
category airplanes manufactured after 4 years or more after the
publication date of the final rule must meet the same standards that
those components must meet when installed in transport category
airplanes with 19 or fewer passenger seats. Those standards, which
involve testing with Bunsen burners, are not to be confused with the
Ohio State University (OSU) radiant rate of heat release testing
required for large-surface-area components installed in airplanes with
20 or more passenger seats. (See proposed Sec. 121.2(e)(2)(ii).)

Comments: ALPA supports the proposed retroactive requirements,
including this proposal.

Fairchild and AIA present identically worded statements opposing
the proposed requirement that seat cushions would have to comply with
the flammability standards of Secs. 25.853(b) and 121.312(b). In that
regard, they state that they know of no evidence that compliance would
provide a significant safety benefit in 10 to 19 passenger airplanes.
They do not believe that compliance would delay the spread of a fire
enough to be an important factor in survival. In that regard, they note
that the seats in smaller airplanes tend to be lightweight and offer
relatively little mass of material to fuel a fire. Also, they believe
that cabin fires are less likely to occur because the small size of the
cabin restricts the amount of carry-on baggage and makes inappropriate
passenger activity less likely. Finally, they believe that the FAA
would have proposed such rulemaking already if warranted. NATA also
believes the higher flammability standards would not be effective in
smaller airplanes. That commenter asserts the cost of compliance would
be $20,000 per airplane.

Commuter Air Technology observes that the Beech King Air executive
airplanes they modify for commuter air service would not have to comply
in their original executive configuration because they have fewer than
ten seats, yet would have to comply as modified because they have more
than ten seats.

Big Sky Airlines and RAA suggest that the compliance period should
be extended to enable replacement during the routine seat replacement
cycle. One of these commenters quotes a compliance cost of $30,000 for
each 19 passenger airplane.

Mesa does not express support or opposition to the proposal, but
states that compliance would entail $12,000, 36 pounds, and 10 hours
for a Beech 1900C, or $3,400, 38 pounds, and 10 hours for either a
Beech 1900D or Jetstream 3100.

No comments were received concerning the proposal to require
commuter category airplanes produced four years or more after the
effective date to comply with the Bunsen burner test of part 25
(Sec. 25.853(a)). One commenter states that the installation of
interior materials complying with Sec. 25.853(c) would not improve the
level of safety of airplanes with 10 to 19 passenger seats.

FAA Response: The commenters focus on the cost of compliance and
the lack of a need for added fire protection in smaller airplanes.

In regard to costs, the commenters appear to have a misconception
concerning the scope of the rulemaking. The costs fall into one of two
categories--the cost of developing and testing suitable cushion
materials and the actual cost of replacing individual seat cushions. In
regard to the former, Sec. 25.853(c) does not require each seat cushion
to be tested, nor does it require each seat cushion design to be
tested. Instead it simply states that each cushion must meet the
flammability standards. An applicant has the option of utilizing a seat
cushion material that meets the flammability standards;
however, most choose to comply by using a covering material that
protects the cushion from the fire. (The latter are usually referred to
as "fire-blocked seats.") Individual seat cushions or individual seat
cushion designs do not have to be tested if they can be shown to meet
those standards by similarity to other cushions that have been tested
previously and found to meet the standards. Advisory Circular (AC)
25.853-1, Flammability Requirements for Aircraft Cushions, issued
September 17, 1986, provides guidance in that regard. In the years that
have passed since transport category airplanes used in part 121 or 135
service were first required to comply, many different possible seat
cushion designs have already been tested and found satisfactory. It is,
therefore, quite possible to utilize a seat cushion material or fire-
blocking material that has already been shown to comply with the
flammability standards. In that regard, many of the affected airlines
are affiliated with major airlines and have ready access to the same
means of compliance adopted several years earlier by those major
airlines.

Contrary to some commenters' beliefs, the use of seat cushions
meeting these flammability standards is quite effective in the cabins
of smaller airplanes. Some commenters note that the amount of cushion
material is relatively small in 10- to 19-passenger airplanes. While
the amount of cushion material in those airplanes is obviously much
less than that in larger airplanes, it represents approximately the
same portion of the total flammable material in those airplanes as in
the larger airplanes. In addition to representing a large portion of
the materials in the cabin that are flammable, the foam materials
typically used for seat cushions are, by far, the most flammable of all
the materials used in the cabin. A secondary, but no less significant,
benefit is that cushions meeting these flammability standards are much
less likely to ignite and sustain a flame than those that do not meet
the standard. Precluding a fire from occurring is obviously the best
possible form of fire protection.

The FAA conducted a series of 12 full-scale fire tests at its
Technical Center at Atlantic City, New Jersey, using the fuselage of a
Metroliner. The cabin of the Metroliner is typical of those of the part
23 Normal or Commuter Category airplanes with 10 to 19 passenger seats.
Under the test conditions, it was shown that using seat cushions
meeting these flammability standards, in lieu of the flammability
standards that would otherwise be applicable, would afford passengers
approximately 45 additional seconds in which to escape.

The primary benefit of having seat cushions that meet these
flammability standards is to afford occupants more time in which to
egress in a post-crash fire situation; however, such cushions also
provide additional protection should an inflight cabin fire occur.
Contrary to the beliefs of commenters in that regard, the FAA is aware
of at least six instances in which cabin fires have been experienced
since 1980 in nontransport category airplanes or transport category
airplanes with cabins of similar size.

In their recommendation A-88-96, the National Transportation Board
(NTSB) recommended the use of fire-blocking materials on seats in part
23 normal and commuter category airplanes. Fairchild, AIA, and others
state that the fact that the FAA has not previously adopted seat
cushion flammability standards for those airplanes is evidence that
they would not result in a significant improvement in safety. The FAA
has, in fact, initiated separate rulemaking in that regard (Notice No.
93-71, 58 FR 38028, July 14, 1993).

The intent of Notice 95-5 was to mitigate the cost by allowing
compliance to coincide with the normal wear replacement cycles. Since
compliance can be achieved whenever the seat cushions or seat coverings
are being replaced due to normal wear, the cost of compliance for each
seat is just the additional cost of including the fire-blocking layer
along with the covering.

Based on the above, the FAA has decided to adopt the seat cushion
flammability standards of Sec. 121.312(c), but to allow a compliance
period of 15 years after the publication date of this rule. The FAA
felt that the immediate cost of this retrofit would have negatively
affected the industry. By allowing up to 15 years, it should be
possible for all replacements to be scheduled within normal replacement
cycles. An additional benefit of a 15-year compliance period is that
certificate holders can coordinate their compliance with this section
with their plans for meeting other extended compliance times, i.e.,
meeting the performance and accelerate-stop requirements and
installation of a third attitude indicator.

As noted above, the FAA also proposed that the interior
components of nontransport category airplanes newly manufactured 4
years or more after the publication date of the final rule must meet
the same standards that those components must meet when installed in
transport category airplanes with 19 or fewer passenger seats (i.e.
Bunsen burner testing). After reviewing the present requirements,
the FAA determined that the interior components of those airplanes
are already required to meet the same flammability standards for
type certification. Since the standards are identical, it is not
necessary to specify the flammability standards as an additional
requirement for newly manufactured airplanes. Section 121.312(a) has
been amended in the final rule to clarify the applicability of the
flammability standards to nontransport category airplanes used by
affected commuters.

Section 121.312 provides the interior material flammability
standards for airplanes operated under that part. As described above,
the substantive provisions of that section are being retained, and the
provisions applicable to airplanes being brought over from part 135 are
being incorporated. In this final rule, Sec. 121.312 is reorganized to
highlight the applicable provisions and to provide greater clarity; the
appropriate substantive text has been retained. Furthermore, appendix L
is being added to part 121 to explain the regulatory citations for the
part 25 provisions that have been superseded. Although those standards
are not current insofar as new type certification under part 25 is
concerned, they are referenced in part 121 and remain applicable for
compliance. The addition of appendix L only clarifies existing
requirements; therefore, it is adopted without prior notice and
comment.

Miscellaneous Equipment. Notice 95-5 specifically discussed the
proposal that would require affected commuters to comply with the
miscellaneous equipment requirements of Sec. 121.313(f) and (g).
However, although not specifically discussed in Notice 95-5,
Sec. 121.313(c) pertaining to a power supply and distributive system
would also be required.

Comments: Fairchild Aircraft notes that Sec. 121.313(c) requires a
power supply and distribution system that meets the requirements of six
sections of part 25. Because Sec. 121.313(c) does not assign an
effective date to this list of part 25 sections, Fairchild assumes that
it is the current version of each section that would be applicable.
Fairchild also questions whether all airplanes currently operated under
part 121 meet the current standards of part 25. Based on their
assumption that their airplanes would have to meet current sections of
part 25 and the fact that SFAR 23 and SFAR 41 airplanes do not meet
those requirements, Fairchild proposes amending Sec. 121.313(c) to
except nontransport category airplanes type certificated after December
31, 1964, from this requirement.

FAA Response: The commenter has correctly identified the sections
of part 25 that are listed in Sec. 121.313(c): however, the commenter has
apparently overlooked the alternative provisions contained in that
section. In part, Sec. 121.313(c) also reads: "or that is able to
produce and distribute the load for the required instruments and
equipment * * * ." This additional text of Sec. 121.313(c) allows the
use of a power supply and distribution system that performs this
function regardless of whether it complies with the listed sections of
part 25. The commenter's proposed amendment is not needed because
Sec. 121.313(c) already includes provisions for alternate means of
compliance. The commenter's products have already been shown to comply
with this alternative.

The commenter is correct in believing that some airplanes currently
operated in part 121 service might not meet the current sections of
part 25 listed in Sec. 121.313(c). The issue is moot, however, since
Sec. 121.313(c) provides for alternative means of compliance.

Cockpit doors and door keys. Section 121.313 (f) and (g) require
that there be a lockable door between the cockpit and the cabin and
that there be a key for each cockpit door that is readily available to
each crewmember. Part 135 does not have such requirements. The FAA
proposed that the affected commuters be required to comply with the
part 121 rules if there is a door with a lock or a door that can be
retrofitted with a lock. (Curtains or accordion doors are not
considered lockable doors.) If a lockable door already exists or can be
retrofitted, the certificate holder would be required to provide a
cockpit key that is readily available to each crewmember. Accordingly,
the language of Sec. 121.313(f) was changed to except nontransport
category airplanes certificated after December 31, 1964, without a
door. Transport category airplanes already are required to have a door
and a lock with a key.

Comments: Most of the comments received on this issue oppose the
requirement for a locking cockpit door and key. Several commenters say
that the cockpit door on EMB-120 airplanes cannot be locked when the
observer jumpseat is in use. These commenters are concerned that strict
adherence to the wording of the rule would require them to retrofit the
door, redesign the cabin, and probably remove a revenue seat, all at a
high cost. These commenters recommend that the EMB-120 be exempted from
the requirement when the observer jump seat is in use. One commenter
states that some nontransport category aircraft that will transition to
part 121 do not have a cockpit door lock and key and may not be able to
install one. One commenter states that operators will be required to
obtain a supplemental type certificate to retrofit airplane doors with
key locks. Another commenter states that this requirement would force
operators to choose between removing the high-quality cockpit door
installed at great expense on BE 1900D aircraft which provides
protection from cabin illumination glare during night operations, or
installing and using a lock on this door, both of which are contrary to
safety. One commenter states that the 1900C and 1900D airplanes have
frangible doors between the cockpit and cabin to reduce distractions.
According to the commenter, as proposed, the rule would require
installation of locks on those doors. Finally, one commenter says that
the wording of the cockpit door requirement should be clarified to
exclude 10 to 19 seat aircraft not yet produced. According to the
commenter, the proposal resolves the problem for existing 10-19 seat
airplanes. However, proposed Sec. 121.2(f) would require all new
airplanes to be certificated in transport category. The commenter
states that new 10-19 passenger airplanes will have the same problem as
existing nontransport category types; that is, cockpit doors will
neither be practical nor appropriate. The commenter recommends amending
Sec. 121.313(f) to read "* * * except that airplanes type-certificated
for a maximum of 19 or fewer passengers are not required to comply with
this paragraph."

AACA notes that the language of Sec. 121.313(f), which lists
required equipment for operating an aircraft, should be changed to
exclude airplanes that do not have cockpit doors.

FAA Response: The FAA maintains that the cockpit key and door lock
requirement should be retained to enhance aviation safety. However, the
final rule language is clarified to require compliance only for
airplanes with a passenger-seating configuration of 20 or more seats.
Therefore, the requirement for a door lock and cockpit key does not
apply to nontransport category airplanes type certificated after
December 31, 1964 even if the airplane has a cockpit door.

In response to the comments regarding the EMB-120, Sec. 121.587
allows for the door to remain open, if necessary, to provide access for
a person authorized admission to the flightcrew compartment. This
allows for the door to be open if the jump seat is in use by an
authorized person. Section 121.587 applies to large airplanes which
includes the EMB-120.

The FAA acknowledges that the commenters correctly state that
keyless locks in airplanes with a passenger seating configuration of 20
or more would have to be retrofitted to work with keys. Certificate
holders that would have to retrofit their door locks would incur a
higher cost to comply with the requirement. Yet, the FAA strongly
believes that keyless locks which only lock from the cockpit side pose
a severe safety hazard if the pilots become incapacitated. The FAA
maintains that an extended time period to retrofit locks is not
justified in light of the many other new requirements which are even
broader in scope.

Cargo and baggage compartments. Part 25 (as referenced in
Sec. 121.314) contains requirements for cargo or baggage compartment
liners, smoke detection, and fire extinguishment for various classes of
compartments. The compartment classification system, also duplicated in
Sec. 121.221 (which as previously discussed applies only to certain
airplanes type certificated before November 1, 1946), is based on the
compartment's accessibility for fire detection and extinguishment. Part
25 was amended in 1989 to require the liners of Class C and D
compartments to meet more stringent flammability standards. Section
121.314 was also adopted at that time to require the improved liners in
existing transport category airplanes on a retroactive basis.

Part 23 contains no classification system or requirements for
compartment fire protection; however, a proposed rule to add comparable
requirements was issued on July 22, 1994 (59 FR 37620). The FAA
proposed in Sec. 121.2(e)(2)(ii) by referencing Sec. 121.314 to require
this modification for commuter category (or its predecessor) airplanes
manufactured 4 years or more after the publication date of the final
rule. However, in Notice No. 95-5, the FAA did not propose to amend
Sec. 121.314, which currently applies only to transport category
airplanes.

Comments: Two commenters submitted identical comments concerning
this proposal. Both commenters believe that the cargo or baggage
compartment classification system of Sec. 25.857, referenced in
Sec. 121.314, is not suitable for smaller airplanes with fewer than 20
seats and that the smoke detector and fire extinguisher requirements
are unreasonable and unnecessary in those airplanes. In that regard,
they note that many commuter category airplanes are convertible from a
full passenger configuration with a relatively small baggage
compartment to combination passenger/cargo (combi) configurations
to cargo only. They do not believe that it is practical to modify any
of the combi configurations to comply with any of the cargo compartment
classes defined by Sec. 25.857. They assert there has been no history
of service problems indicating a need for such features.

No comments were received concerning compartments other than those
of combi airplanes. Also, no commenters responded to the request in the
preamble to Notice No. 95-5 for information concerning less-costly
alternatives such as requiring only liners and smoke detection.

FAA Response: The FAA agrees that the present requirements of
Sec. 25.857 are not entirely suitable for airplanes with a passenger
seating capacity of less than 20 and the FAA has initiated a rulemaking
project to develop and propose similar standards that would be suitable
for these airplanes. In view of this project the FAA has decided to
defer this proposal for future rulemaking.

Fuel tank access covers. As a result of the 1985 Manchester British
Air Tours accident (in which a piece of metal from the aircraft engine
punctured the fuel tank access panel and created a fire),
Sec. 25.963(e) was amended in 1989 to require that all covers located
in an area where a strike by foreign objects is likely must have as
much resistance to fire or debris penetration as the surrounding
structure. Concurrent with the part 25 amendment, Sec. 121.316 was
amended to require airplanes already in service to comply with
Sec. 25.963(e) on a retrofit basis. These requirements pertain to all
transport category, turbine-powered airplanes. Due to their smaller
size and turbo-propeller configuration, part 23 airplanes generally do
not present the same hazard. The FAA did not propose to require part 23
airplanes to comply with Secs. 25.963(e) and 121.316. Since
Sec. 121.316 applies only to "turbine-powered transport category"
airplanes, no rule change is needed. The FAA points out that turbine-
powered transport category airplanes previously operated under part 135
would have to comply with Sec. 121.316.

Comments: Raytheon Corporation submitted comments on the costs of
complying with Sec. 25.963(e) for airplanes that in the future would be
required to be type certificated in the transport category under part
25.

FAA Response: As previously discussed, the applicability of all
present part 25 requirements to airplanes with a passenger seating
capacity in the 10-19 range for which a type certificate is applied for
after March 29, 1995, will be dealt with in a future rulemaking action.
Since Notice No. 95-5 did not propose any change for airplanes in
existence or for airplanes newly manufactured under existing type
certificates, this issue need not be discussed further in this
rulemaking.

Passenger information. Notice 95-5 proposed that affected commuters
would comply with the passenger information requirements in
Sec. 121.317. There was no preamble discussion of this section because
the FAA determined that current requirements for affected commuters in
Secs. 135.127 and 91.517 were substantively the same as those in
Sec. 121.317.

Comments: Three comments were received on this section. Commuter
Air Technology suggests that seatbelts should be worn the entire time
for flights of less than an hour and a half. According to the
commenter, requiring seatbelts at all times while engines are running
would provide better passenger safety, remove an unnecessary checklist
item from the flight station, and eliminate the probability of missing
a flight due to an inoperative sign. According to the commenter, each
seat could be placarded and the co-pilot could make a visual check of
passenger compliance after closing the door hatch prior to departure.

Two commenters state that Sec. 121.317(a) should be revised to
allow permanently lighted no-smoking signs or conspicuous placards,
since smoking is prohibited on all flights.

FAA Response: Section 121.317 sets minimum requirements. Both
Secs. 121.317 and 135.127 allow the use of no smoking placards that
meet the requirements of Sec. 25.1541 if the placards are posted during
the entire flight segment. Section 121.317(a) requires passenger
information signs (fasten seatbelt signs and no smoking signs) that the
pilots can turn on and off and Sec. 121.317(b) specifies when fasten
seatbelt signs must be turned on. To ensure that the present
requirements of Sec. 121.317 are not interpreted so as to prohibit the
use of placards in certain airplanes, a clarifying amendment is
included in the final rule. New Sec. 121.317(l) provides that a person
may operate a nontransport category airplane type certificated after
December 31, 1964, having a passenger-seating configuration of 10-19
seats manufactured before 15 months after the publication date of this
final rule if it is equipped with one placard that is legible to each
person seated in the cabin that states "Fasten Seat Belt" if the
flightcrew orally instructs the passengers to fasten their seatbelts at
the necessary times. Newly manufactured airplanes must comply with
lighted seat belt sign requirements of Sec. 121.317(a) within 2 years
after the date of publication of this final rule. In addition,
Sec. 121.317(d) requires one legible sign or placard that reads
"fasten seat belt while seated" that is visible from each passenger
seat. Affected commuters must comply with Sec. 121.317(d) at the time
of recertification under part 121, or within 15 months, whichever
occurs first.

Instruments and equipment for operations at night. Section 121.323
requires two landing lights for night operations. Under the proposal,
the requirement would apply to all affected commuters. While no
comments were received on the proposal, the FAA had intended to revise
Sec. 121.323 to except nontransport category airplanes certificated
after December 31, 1964, from having more than one landing light. The
exception was intended because small airplanes with shorter wing spans
can be operated safely with only one landing light. The exception was
inadvertently omitted from Notice 95-5 but is included in the final
rule.

Oxygen requirements. Sections 121.327 through 121.335 cover
supplemental oxygen requirements and oxygen equipment requirements. The
requirements are similar to the oxygen requirements in Sec. 135.157
except that for certain airplanes, part 121 requires less oxygen. Each
affected commuter who would have to comply with part 121 oxygen
requirements as a result of this rulemaking should be able to operate
its airplanes in accordance with the oxygen requirements specified in
part 121.

Comments: Fairchild Aircraft comments that the first aid oxygen
requirements of Sec. 121.333(e)(3) are inappropriate for smaller
commuter service and that this section should be revised to exclude
airplanes with fewer than 20 seats. This commenter also asks that
Sec. 121.335 be revised to allow oxygen flow rates based on the
airplane's certification basis rather than Civil Air Regulation 4b.651.
Fairchild finds that this would avoid unnecessary complication and
expense.

FAA Response: In the case of first aid oxygen, since Notice 95-5
proposed no flight attendant for the 10- to 19-seat airplane, requiring
the first aid oxygen that would be dispensed by a flight attendant
would not be logical. Since the airplanes operated by the affected
commuters were not type certificated for flight above 25,000 feet and
since Sec. 121.333(e)(3) only applies to pressurized airplanes that
operate above 25,000 feet, it would not as a practical matter apply to
commuter (or predecessor) airplane operations. The requirement does
apply to airplanes with 20 to 30 passenger seats, as proposed.

In the case of Sec. 121.335, the FAA finds that parts 23 and 25
provide standards for oxygen that either meet or exceed the standards
in section 4b.651 of the CAR. Section 4b.651 has a built in deviation
authority.

Portable oxygen for flight attendants. Section 121.333(d) requires
that each flight attendant shall, during flights above 25,000 feet,
carry portable oxygen equipment with at least a 15-minute supply of
oxygen, unless enough portable oxygen units with masks or spare outlets
and masks are distributed through the cabin to ensure immediate
availability of oxygen to each flight attendant regardless of his or
her location at the time of cabin depressurization. Part 135 does not
have a similar requirement for portable oxygen for flight attendants.
In Notice 95-5, the FAA proposed that affected commuters who use flight
attendants in their operations and that operate above 25,000 feet be
required to comply with the part 121 requirement. No comments were
received on this issue and the final rule is adopted as proposed. For a
related discussion on the use of oxygen, see the discussion under
"Oxygen Requirements."

Protective breathing equipment (PBE). Section 121.337 contains
requirements for equipping the flight deck and passenger compartments
of transport category airplanes with PBE. Part 135 does not currently
require any type of PBE.

Section 121.337(b)(8) (smoke and fume protection) requires PBE,
either fixed or portable, to be conveniently located on the flight deck
and easily accessible for immediate use by each flight crewmember for
smoke or fume protection at his or her duty station. In addition,
Sec. 121.337(b)(9) (fire combatting) requires that for combatting fires
a portable PBE must be located on the flight deck with easy access by
each flight crewmember for fighting fires. Also portable PBE in the
passenger compartment must be located within 3 feet of each hand fire
extinguisher. Both of these requirements provide that the Administrator
may authorize another location if special circumstances exist that make
compliance impractical and the proposed deviation would provide an
equivalent level of safety.

The proposal required affected commuters to comply with the PBE
requirements of Sec. 121.337. To be in compliance, an airplane with a
passenger-seating configuration of 10 to 19 seats would have to have at
least three PBE: one PBE, fixed or portable, for each flight crewmember
at his or her station, and an additional portable PBE on the flight
deck for use in fighting fires. An airplane with a passenger-seating
configuration of 20 to 30 seats would have to have at least four PBE:
one PBE, fixed or portable, for each flight crewmember at his or her
station; an additional portable PBE on the flight deck for fighting
fires; and a portable PBE in the passenger compartment located within 3
feet of the required hand fire extinguisher.

The proposal revised the applicability of the current rule to
include other than transport category airplanes. Proposed
Sec. 121.337(b)(9)(iv) was also revised to except airplanes having a
passenger-seating configuration of fewer than 20 seats and a payload
capacity of 7,500 pounds or less from the requirement to have a PBE in
the passenger compartment. The exception is needed because these
airplanes are not required to have a flight attendant; for these
airplanes, the portable PBE on the flight deck could be used by a
flight crewmember for fighting a fire.

The FAA proposed to require compliance with Sec. 121.337 by a date
2 years after the publication date of the final rule. (See Sec. 121.2)

Comments: Several commenters oppose the PBE requirement. These
commenters are concerned about the lack of space in the plane, the high
compliance cost, and the lack of benefits in having the equipment.
These commenters state that PBE equipment on non-pressurized aircraft
is not justified. Two commenters claim that their current equipment
(built in oxygen supply systems and masks) ought to exempt them from
the PBE requirement. One commenter incorrectly believes that a PBE
would be required for the cabin on METRO aircraft (a 19 seat airplane).
One commenter suggests that in the interest of safety the FAA should
reduce the compliance time for PBE equipment to 6 months. Though
commenters provide cost estimates to install PBE on their airplanes,
costs are provided only for 10 to 19 seat airplanes, which would not be
required to have PBE in the cabin.

FAA Response: The FAA maintains that the proposed PBE requirement
for affected commuters is appropriate. There are several safety
benefits for requiring smoke and fume PBE. The use of smoke and fume
PBE required by Sec. 121.337(b)(8) would help prevent the injury or
death of flight crewmembers from smoke or harmful gases.

The FAA contends that there is adequate space in the cabin of 20-
to 30-seat commuter airplanes to accommodate portable PBE for fire
combatting, and no major cabin retrofits would be required. With regard
to firefighting PBE, the FAA has determined that such equipment is not
appropriate for operations with 10-19 passengers. There are no flight
attendants on these flights and the pilots generally remain on the
flight deck to operate the aircraft during an emergency. In an
emergency, passengers will have access to a fire extinguisher and will
be able to assist in extinguishing any flames within the cabin.
However, passengers are not trained in the use of fire combatting PBE
and would not know how to operate such equipment. Accordingly,
nontransport category airplanes type certificated after December 31,
1964, having a passenger-seating configuration of 10- to 19-seats are
excepted in the final rule from the requirements in Sec. 121.337(b)(9)
for having PBE's for combatting fires.

In response to other comments, the lack of a pressurized cockpit
does not diminish the need for PBE to enhance safety in case of fire,
nor can existing oxygen systems provide adequate protection for
fighting a fire. Approved PBE in the cabin must have a protective hood
and be fully mobile.

Due to the broad scope of this rulemaking action, certificate
holders will have to deal with many new requirements. Therefore, as
proposed, a consistent compliance period of 2 years is applied to all
affected airplanes for acquiring PBE.

Emergency equipment for extended overwater operations. Sections
121.339 and 135.167 require that airplanes engaged in extended
overwater operations (more than 50 nautical miles from the nearest
shoreline) provide the following: enough life rafts of a rated capacity
and buoyancy to accommodate the occupants of the airplane; a life
preserver equipped with an approved survivor locator light for each
occupant of the airplane; a pyrotechnic signaling device for each life
raft; a survival kit and a survival type emergency locator transmitter.
In addition, Sec. 121.339 requires that unless excess rafts of enough
capacity are provided, the buoyancy and seating capacity of the rafts
must accommodate all occupants of the airplane in the event of loss of
one raft of the largest rated capacity. In practice, this requirement
is typically met by carrying a spare raft of the largest rated
capacity.

The FAA proposed that the affected commuters that engage in
extended overwater operations should be required to meet the part 121
requirements. As with current part 121 certificate holders, affected
commuters can apply for deviations, and the FAA can decide, on
a case by case basis, if a deviation is appropriate. These deviations
are issued pursuant to Sec. 121.339(a) which permits the Administrator
to allow deviation from the requirement to carry certain equipment for
extended overwater operations. Since there are few extended overwater
operations conducted by commuters, the FAA does not expect this
proposed requirement to have a significant impact.

Comments: Four commenters argue against the requirement for a spare
life raft on commuter airplanes. One commenter says that the spare life
raft is not necessary because seats can be equipped with additional
life vest storage pouches. Another commenter says that the spare life
raft is appropriate for larger airplanes but not for 10 to 30 seat
aircraft. This commenter also suggests that the rule should remain as
presently written under Sec. 135.167, and, on a case-by-case basis, the
FAA can require certificate holders to obtain a spare life raft.
Another commenter states that spare life rafts should not be required
on aircraft with less than 20 passenger seats because the requirement
will increase operating costs and reduce passenger revenues. A fourth
commenter states that the cumulative weight, space, and compliance
costs will be significant for affected Alaskan operators and that these
costs cannot be spread across a large number of passenger seats as can
be done with a larger aircraft.

Three commenters state that the requirement in Sec. 91.205 (b)(11)
for a pyrotechnic signaling device is understandable for general
aviation aircraft, but is impractical and superfluous for airplanes
operating under part 121 in scheduled air carrier service. The
commenters recommend that Sec. 91.205 be revised to exclude airplanes
operating under part 121.

FAA Response: The FAA maintains that airplanes conducting extended
overwater flights need to carry enough life rafts to accommodate all
passengers in the event of the loss of the life raft with the largest
rated capacity. Such a requirement will enhance safety in the event of
an accident. Individual flotation devices are not adequate for safety
in the event of a water ditching because passengers tend to separate in
open water. A life raft enables passengers to stay together. An even
greater threat is hypothermia, a sequence of physical reactions
resulting from the loss of body heat. In cold water, a person will
experience increased difficulty with mobility and intense shivering
occurs. In arctic waterways, survival time can be as little as 2 or 3
minutes. Thus, a spare life raft is appropriate for affected commuters
to enhance passenger safety. The requirement in part 121 for equipping
each life raft with a pyrotechnic signaling device is identical to part
135 for extended overwater operations. The recommendation to except
scheduled air carriers from the provisions of Sec. 91.205(b)(11) is
beyond the scope of this rulemaking. Moreover, under Sec. 119.1(c)
persons subject to part 119 must comply with other requirements of this
chapter, except where those requirements are modified by or where
additional requirements are imposed by parts 119, 121, 125, or 135 of
this chapter. Therefore, the final rule requires commuter airplanes to
adhere to part 121 standards and provides deviation authority on a case
by case basis.

Flotation devices. Section 121.340 requires that a large airplane
in any overwater operation must be equipped with life preservers or
with an approved flotation means for each occupant. Because it is
practically impossible to operate any place without flying over a body
of water of sufficient depth to require some sort of flotation means,
Sec. 121.340 has been applied so that virtually every airplane is
equipped with either flotation cushions or life preservers. In parts
121 and 135, life preservers are required only for extended overwater
operations, (Secs. 121.339 and 135.167). Therefore, airplanes used in
extended overwater operations are already equipped with life preservers
and do not need to have flotation cushions.

The FAA proposed that airplanes equipped with 10 or more seats
operating in scheduled passenger operations would comply with
Sec. 121.340 and accordingly proposed revising the section to delete
the word "large." To allow any replacement of seat cushions to be
coordinated with the seat cushion flammability requirements of
Sec. 121.312(c), the FAA proposed a compliance date of 2 years after
the publication date of the final rule.

Comments: The FAA received three comments that oppose the
requirement for flotation devices. One commenter opposes the
requirement because of the equipment cost and weight penalty. This
commenter determines that the seat cushions in the METRO aircraft would
not serve as effective flotation devices. The commenter provides a cost
estimate for acquiring and retrofitting individual flotation devices
for METRO airplanes. The commenter also states that each flotation
device for 10 to 30 seat airplanes would have to be equipped with an
approved survivor location light. A second commenter states that the
rule should allow exemptions for operations that do not fly over or
near large bodies of water. This commenter does not believe that
flotation devices would enhance safety. Finally, a third commenter
states that flotation devices are already required for extended
overwater flights for all airplanes by Sec. 91.205.

FAA Response: The FAA concurs that if the seat cushions in a
particular airplane model do not serve as flotation devices, then
individual flotation devices would have to be acquired. If life
preservers are provided as individual flotation devices they would have
to have an approved survivor locator light as required by
Sec. 121.339(a)(1).

The FAA found during previous rulemaking that all flights traverse
a body of water of at least 6 feet deep during the course of a year.
Therefore, individual flotation devices or life preservers for 10 to 30
seat airplanes are required on all flights. Section 121.340(b) contains
provisions for requesting an approval to operate without the flotation
means if the operator shows that the water over which the airplane is
to be operated is not of such size and depth that life preservers or
flotation devices would be needed for survival.

The FAA concurs with one of the commenters that Sec. 91.205
requires flotation devices for all airplanes involved in extended
overwater flights. Section 121.340 is clearly more restrictive.

Although the compliance date for meeting passenger seat cushion
flammability requirements has been extended to 15 years, the compliance
time of 2 years for providing flotation devices is the same as
proposed.

Equipment for operations in icing conditions. Section 121.341
requires certain equipment for operations in icing conditions. The
proposal would require affected operators to comply with this section.
In accordance with Sec. 121.341(b), to operate an airplane in icing
conditions at night, a wing ice light must be provided or another means
of determining the formation of ice on the parts of the wings that are
critical from the standpoint of ice accumulation. This would be a new
requirement for 10- to 19-passenger seat airplanes.

No comments were received on this proposal; however, the FAA has
determined that the requirements of Sec. 135.227 (c), (e), and (f) need
to be incorporated into Sec. 121.341 to accommodate certain affected
airplanes. These requirements pertain to operating limitations for
flying into known icing conditions if the airplane is not
equipped for icing conditions. Thus the final rule Sec. 121.341
incorporates the part 135 language.

Pitot heat indication system. Section 25.1326 requires a pitot heat
indication system to indicate to the flightcrew when a pitot heating
system is not operating. Part 23 currently requires pitot heat systems
for airplanes approved for IFR flight or flight in icing conditions,
but does not require pitot heat indicators. Section 121.342 currently
requires a pitot heat indication system on all airplanes that have
pitot heat systems installed.

In recommendation A-92-86, the National Transportation Safety Board
(NTSB) recommended that small airplanes certificated to operate in
icing conditions and at altitudes of 18,000 feet mean sea level and
above should be modified to provide a pitot heat operating light
similar to the light required by Sec. 25.1326. As recommended by the
NTSB, the FAA proposed to amend part 23 to require such indication for
commuter category airplanes (Notice No. 94-21, 59 FR 37620, July 22,
1994). This new requirement, when adopted, will apply to new type
certification and will not affect existing in-service commuter
airplanes or future production of currently approved commuter
airplanes.

In Notice 95-5, the FAA proposed to amend Sec. 121.342 to require
nontransport category airplanes type certificated after December 31,
1964, to incorporate pitot heat indication systems. Affected commuters
would have to comply within 4 years after the publication date of this
rulemaking.

Comments: Three comments were received on this proposal. Fairchild
Aircraft Co., a manufacturer of commuter airplanes fully supports the
proposal.

RAA notes that FAA's cost estimate of $500 was significantly lower
than the commenter's estimate of between $1,500 and $25,000 per
airplane. The commenter further states that there was no known history
of accidents or incidents to justify the cost of retrofits and
recommends that the requirement apply only to newly manufactured
airplanes.

Commuter Air Technology, an aircraft modifier, notes that pitot
tubes are accessible to ground personnel who could ascertain their
proper function prior to flight. The commenter argues that because of
the short duration of commuter flights (usually 1 hour) failure in
flight would probably allow for continued flight to the next airport.

FAA Response: As a result of comments received in response to
Notice 95-5, the FAA re-examined the cost estimates of this rulemaking.
Those revised cost estimates, which are higher than those in the
proposal, are included in the Regulation Evaluation Summary of this
rulemaking.

The FAA disagrees with the commenter's contention that ground
checks and short flights preclude the need for pitot tube heat
indicators. Airspeed indicating errors caused by unheated pitot tubes
have contributed to icing-related accidents. Airspeed indicating errors
are not always obvious to the pilot who may make decisions based on the
resulting erroneous information. A system which indicates when the
pitot tube is, or is not, heated will provide the crew with the status
of the system.

Therefore, the FAA is amending Sec. 121.342, as proposed, to
require nontransport category airplanes type certificated after
December 31, 1964, that are equipped with a flight instrument pitot
heating system to incorporate pitot heat indication systems within 4
years after the effective date of this rulemaking.

Flight data recorders (FDR's). Notice 95-5 did not propose any
substantive revisions to current part 121 or part 135 flight data
recorder (FDR) requirements. According to the proposal, affected
commuters would continue to meet part 135 requirements while the FAA is
developing updated FDR requirements for both parts 121 and 135.

Comments: One commenter states that some of the current equipment
being used is providing inadequate records and that part 121 and 135
certificate holders should be required by December 31, 1999, to install
new FDR on all airplanes. He further states that industry data
indicates the changeover will cost $29 million divided by 454 million
passengers a year, and that equates to 6 cents increase in ticket
prices.

AIA and Raytheon state that following NTSB safety recommendations
on FDR's could result in as large an impact on the economic viability
for current and future aircraft in this category as the effects of
Notice 95-5. They further state that although additional information
from FDR's is needed, the safety recommendations as written would
require 56 to 84 channels of data on a 1900D and would be excessive for
most data requirements. This would result in a large redesign effort
and related increases in costs.

American Eagle comments that it believes that this equipment, as
well as cockpit voice recorders, is important in the post-incident
investigation process and, as a result, has installed FDR's on all its
aircraft even though not all aircraft operated under part 135 are
required to have them. It strongly supports extending the current part
121 requirement to all aircraft with 10 or more seats operating in
scheduled passenger service. In addition, the commenter supports
regulations which would require such equipment to meet a new, higher
minimum standard.

FAA Response: A recommendation for a rule change on FDR's is being
addressed by the Aviation Rulemaking Advisory Committee (ARAC), and the
concerns of the commenting parties will be reflected in that separate
rulemaking if a rule change is proposed. This rulemaking did not
propose any increase in channels for existing FDR's.

For clarification the proposed rule language has been revised in
Sec. 121.344 of the final rule to state that Sec. 135.152 FDR
requirements will apply to airplanes with a payload capacity of 7,500
pounds or less and a passenger seating configuration, excluding any
pilot seat, of 10-30 seats. The proposed rule had not specified
passenger seating capacity.

Radio equipment. Sections 121.345 through 121.351 cover radio
equipment requirements. Part 121 specifies radio equipment requirements
for operations under VFR over routes navigated by pilotage, for
operations under VFR over routes not navigated by pilotage or for
operations under IFR or over-the-top, and for extended overwater
operations. The requirements are more specific and restrictive than
those in Sec. 135.161. The radio equipment requirements in part 121 are
cumulative; that is, the regulations prescribe basic radio equipment
requirements for VFR over routes navigated by pilotage and additional
equipment for VFR over-the-top or IFR. Almost all part 121 operations
are conducted under IFR. The proposed rule would require affected
commuters to comply with part 121 radio equipment requirements.

The final rule revised Sec. 121.349 (radio equipment for operations
under VFR over routes not navigated by pilotage or for operations under
IFR or over the top) by adding a new paragraph (e) which incorporates
requirements in Sec. 135.165(a). This change is necessary because part
121 does not have comparable requirements.

Emergency equipment for operations over uninhabited terrain.
Section 121.353 prescribes the emergency equipment needed for
operations over uninhabited terrain for flag and supplemental
operations. The requirements include pyrotechnic signaling devices,
emergency locator transmitters (ELT's), and survival kits equipped for
the route to be flown. The proposed rule would require
compliance with Sec. 121.353.

Comments: Two commenters state that application of Sec. 121.353 to
affected commuters would provide relief from compliance with
Sec. 91.205, which would reduce the standards. One of these commenters
claims that S-type ELT's as required by Sec. 121.353 are useful for sea
ditching but are of no use over uninhabited terrain. According to the
commenter, they are intended for extended overwater operations, are
immersion activated, are not intended for fixed installation on
aircraft, lack any impact G-force activation feature, are very bulky,
are extremely expensive, and, by design, are not suitable for surviving
situations other than sea ditching. The commenter states that
incapacitated survivors on uninhabited terrain cannot expect any help
from an S-type ELT. The commenter recommends revising Sec. 121.353 to
state that the provisions are in lieu of part 91 provisions and that an
airplane subject to part 121 must be equipped with an ELT or
pyrotechnic signal device in accordance with Sec. 121.353 or
Sec. 121.339 (extended overwater).

RAA also states that the requirement for pyrotechnic signaling
devices is impractical for airplanes operating under part 121 and
recommends that Sec. 91.205(b)(11) be amended to exclude these
certificate holders.

RAA and ASA point out that the requirement for ELT's in Sec. 91.207
exempts turbojet-powered aircraft and aircraft engaged in scheduled
flights by scheduled air carriers. RAA and ASA believe that all jet-
powered airplanes that normally operate under part 121 whether or not
they utilize propellers should be exempt from the requirements of
Sec. 91.207 during flight operations under part 91, such as ferry,
training, testing, proving runs, which are incidental to or in support
of scheduled operations. RAA and ASA recommend revising
Sec. 91.207(f)(1) to read: "Large turbine powered airplanes."

AACA indicates that the economic analysis did not include the
weight penalties or costs for installing, maintaining, repairing, and
training for the use of survival kits. AACA also states that the rule
is unclear as to when the kits are required since "uninhabited areas"
is not defined. AACA recommends clarifying the applicability of these
requirements to Alaska. AACA, as well as other commenters, also states
that there is an Alaskan state law requiring extensive survival
equipment on board any aircraft operated in the State.

FAA Response: In response to the applicability to Alaska, although
scheduled intrastate operations within the States of Alaska and Hawaii
are currently conducted under flag rules, as a result of this final
rule, these will now be domestic operations and the survival equipment
requirements do not apply to domestic operations. The FAA did not
intend to reduce requirements for operations over uninhabited terrain
in Alaska or Hawaii as currently applicable. Therefore, the title of
Sec. 121.353 has been revised and an applicability statement added to
include Alaska and Hawaii. Since these operators have been meeting flag
requirements, this revision will not be a change for them.

The revisions requested to part 91 to exempt ferry flights and
other types of flight incidental to scheduled flights is a separate
issue from the requirements of Sec. 121.353 which pertain only to
emergency equipment for operations over uninhabited terrain. Any
amendment to part 91 would need to be part of a separate rulemaking.

The FAA does not agree that the language of Sec. 121.353 should be
revised to clarify that it replaces the requirements for pyrotechnic
signaling devices in Sec. 91.205(b)(11) pertaining to aircraft for hire
operated over water beyond power off gliding distance to shore. The
proposed applicability of Sec. 121.353 to affected commuters if they
fly a supplemental or flag operation does not affect the applicability
of part 91 requirements. The requirements of Sec. 91.205(b)(11) would
continue to apply under applicable circumstances. Part 121 requirements
are in addition to part 91, not in lieu of part 91.

The FAA does not agree with the commenter's claim that survival-
type ELT's do not work except in water ditchings. It is true that S-
type ELT's must meet certain buoyancy, waterproofness, and immersion in
salt water requirements. While many S-type ELT's employ water-activated
batteries, they are not required. Regardless of the type of battery
used, each ELT must have a means by which it can be activated manually.

In addition, this rulemaking does not define "uninhabited
terrain." When the predecessor regulation to Sec. 121.353 was proposed
in CAB draft release 58-24 in 1960, "uninhabited terrain" was defined
as "flights for long distances over frigid or tropical land areas for
which the Director finds such equipment to be necessary for search and
rescue operations because of the character of the terrain to be flown
over." When the rule was adopted, the wording was changed to provide
the Administrator more flexibility in identifying uninhabited areas.
Since implementation is on a case-by-case basis through operations
specifications, it was determined that the proposed wording was not
necessary. This provision has been in effect for over 30 years without
any problem about the meaning of "uninhabited areas."

Airborne weather radar. The proposed rule would require all
affected commuters to have airborne weather radar in accordance with
Sec. 121.357. Currently, part 135 requires weather radar for 20-30
passenger seat airplanes and weather radar equipment or approved
thunderstorm detection equipment for 10-19 passenger airplanes.

Comments: Three comments were received on the proposal. RAA and AMR
Eagle support the proposed requirement. AMR Eagle states that commuter
operations are typically characterized by high frequency operations at
lower altitudes with short stage lengths which necessarily limits
preplanning, planning, or executing a desired deviation in flight
profile because of changing weather. Hence a flightcrew needs all
available tools to conduct safe operations.

One commenter states that airborne weather radar is not needed in
Alaska because severe thunderstorms and tornadoes do not occur there.

AACA claims that Notice 95-5 is silent about the exceptions for
operations within the states of Alaska and Hawaii and within parts of
Canada. AACA requests that the FAA specifically address the issue that
airborne weather radar and airborne thunderstorm detection equipment
will not be required for operations previously excepted under part 121
and part 135 (Secs. 121.357(d) and 135.173(e)). According to the
commenter, there have been no meteorological changes in Alaska since
the regulation was originally written; therefore, this equipment is no
more necessary now than it ever was.

FAA Response: The FAA agrees with AACA that, in accordance with
Sec. 121.357(d), airborne weather radar is not required for airplanes
used solely within the State of Hawaii or the State of Alaska or that
part of Canada west of longitude 130 degrees W, between latitude 70
degrees N and latitude 53 degrees N, or during any training, test, or
ferry flight. This exception is retained in the final rule. In Notice
95-5 the FAA did not propose to delete the Sec. 121.357(d) exception.

All other affected operators would have to have airborne weather
radar within the 15-month compliance period.

Traffic Alert and Collision Avoidance System (TCAS). Under the
proposal, affected carriers would be required to comply with part 121 TCAS
requirements in Sec. 121.356. There are no substantive differences
between part 121 and part 135 TCAS requirements for aircraft with
passenger seating configurations of 10-30 seats.

Comments: Fairchild Aircraft recommends that the words,
"combination cargo" be deleted from Sec. 121.356(b).

ALPA says that the FAA should require TCAS II for aircraft with
fewer than 30 passenger seats, including cargo aircraft (which have
increased in recent years).

RAA recommends revising Sec. 121.356(a) to require that "* * *
each certificate holder shall equip its airplanes with an approved TCAS
II traffic alert and collision avoidance system and the appropriate
class of Mode S transponder. * * *"

Two certificate holders, Samoa Air and Inter Island Air, say that
TCAS is expensive and useless for their operating environment, i.e.,
airspace with little air traffic.

Fairchild Aircraft states that Sec. 121.345(c)(2), which requires
Mode S transponders, is similar to a requirement in part 135
(Sec. 135.143(c)(2)). According to the commenter, the Mode S equipment
has not been installed and the commenter believes that the FAA is
granting exemptions to the requirement for part 135 certificate
holders. If exemptions would not be granted under part 121, significant
cost would be involved.

FAA Response: The intent of the proposed rule Sec. 121.356 was that
airplanes with a passenger seating configuration of 10 to 30 seats must
be equipped with at least a TCAS I system which is the same as the
present part 135 requirement for the affected airplanes. TCAS I systems
are not required to be equipped with Mode S transponders.

As a commenter states, unrelated to TCAS I requirements, exemptions
to the Mode S requirements of part 135 are currently in effect. Any
affected commuters who hold an exemption from the part 135 requirement
or from Sec. 135.143, Mode S requirements, after this final rule must
reapply to be exempted from the Mode S requirements of part 121.345.

The commenter's recommendation to require TCAS for all-cargo
operations is beyond the scope of this rulemaking, as are the
recommendations to require TCAS II for all airplanes and to exempt
certain affected certificate holders from the requirement for
certificate holders to have TCAS I by December 1995.

Low-altitude windshear systems. Section 121.358 requires an
approved airborne windshear warning system for most turbine powered
airplanes. It specifically excludes turbopropeller-powered airplanes.
No comments were received concerning this section and the final rule is
adopted as proposed. Comments received on windshear training
requirements are discussed under subpart N.

Cockpit voice recorders. No comments were received on this issue;
however, the FAA is making a change in the final rule language to
correctly incorporate the current CVR requirements that apply to
airplanes with 10-30 passenger seats.

Ground proximity warning system (GPWS). Under the proposed rule,
affected commuters would have to comply with the GPWS requirements of
Sec. 121.360. By the compliance date of this rulemaking, all part 135
operators of turbine powered airplanes having a passenger seating
configuration of 10 or more seats would have to have GPWS. All affected
commuters are included in this requirement. The GPWS required under
part 135 would meet the standards of part 121.

No comments were received on this issue; however, the FAA has
discovered that the word "large" was not deleted from Sec. 121.360.
This deletion is necessary if the requirements are to apply to all
affected commuters. Accordingly the word "large" is deleted in the
final rule.

VI.A.8. Subpart L--Maintenance, Preventive Maintenance, and Alterations

Applicability. Part 121 certificate holders are required to adopt a
continuous airworthiness maintenance program (CAMP), which has a proven
track record for large transport category airplanes. Under
Sec. 135.411(a)(2), airplanes that are type certificated for a
passenger-seating configuration of 10 seats or more are already
required to comply with a CAMP similar to part 121 requirements. The
proposed rule would require all airplanes type certificated for 10 or
more passengers to comply with part 121 CAMP requirements. These
requirements are consistent with present-day maintenance standards and
techniques to manage airplane airworthiness. The proposal to include
affected commuters under part 121 maintenance requirements would not
necessitate a revision to Sec. 121.361.

Section 121.361(b) contains a deviation provision allowing certain
foreign noncertificated persons to perform maintenance. Affected
commuters would now have this option available. Since many of the
airplanes that are the subject of this rulemaking are manufactured
outside the United States, this deviation provision would allow
certificate holders to have the original equipment manufacturers
perform some overhauls and repairs.

Comments: Jetstream Aircraft Limited supports the proposals to
apply this subpart to affected commuters.

American Eagle encourages proposed rulemaking which would mirror
current parts 121 and 25 maintenance and inspection requirements for
aircraft certificated under part 23 or SFAR 41 and used in commercial
aviation of any type.

FAA Response: Since the comments in effect support the proposed
rule changes, they are adopted as proposed.

Responsibility for airworthiness. Section 121.363 places the
responsibility for airworthiness of an airplane on the certificate
holder; Sec. 135.413 contains a similar requirement. Under the
proposal, affected commuters must comply with Sec. 121.363. Section
135.413(a) requires a part 135 operator to have defects repaired
between required maintenance under part 43. This provision does not
appear in part 121. Part 121 operators are required to have defects
repaired in accordance with their maintenance manual. Since an FAA-
approved maintenance manual requires no less than the part 43
requirements, affected commuters would experience no change in
requirements under the proposal. On this issue, no comments were
received and the final rule is adopted as proposed.

Maintenance and preventive maintenance, and alteration
organization. Section 121.365 requires the certificate holder to have
an adequate maintenance organization for the accomplishment of
maintenance, preventive maintenance, and alterations on its airplanes.
The provision allows the certificate holder to arrange with another
person to accomplish the work, provided that the certificate holder
determines that the person has an organization adequate to perform the
work. This provision requires separate inspection functions to ensure
that those items directly affecting the safety of flight are verified
to be correct by someone other than the person who performed the work.

The FAA recognizes that other provisions of the proposed rule in
Notice 95-5, which would require affected certificate holders to
install new equipment and might lead to replacement of part 23 type
certificated airplanes with part 25 type certificated airplanes, could
necessitate that maintenance personnel (as required by this section
and by Secs. 121.367 and 121.371) have additional skills
and training.

Comments: American Eagle supports the proposal.

FAA Response: Since the only comment on this issue is supportive,
the rule is adopted as proposed.

Manual requirements. Sections 121.369 and 135.427 have almost
identical requirements specifying that the certificate holder include
in its manual a description of the organization required by
Sec. 121.365 and a list of persons with whom it has arranged for the
performance of any required inspections, other maintenance, preventive
maintenance, or alterations. The manual must contain the programs
required by Sec. 121.367, including the methods of performing required
inspections, other maintenance, preventive maintenance, or alterations.
This manual is necessary to ensure that the certificate holder has
provided an adequate maintenance program for the airworthiness of its
airplanes and to inform its personnel, or other persons who perform
maintenance, of their responsibilities regarding the performance of
maintenance on the airplane. In the proposal, the FAA required affected
commuters to comply with part 121. No comments were received on this
issue and the final rule is adopted as proposed.

Required inspection personnel. Sections 121.371 and 135.429 contain
similar requirements for inspection personnel, including provisions for
specific qualifications for and supervision of an inspection unit.
Included is a requirement for listing names and appropriate information
of persons who have been trained, qualified, and authorized to conduct
required inspections. This requirement ensures that competent and
properly trained inspection personnel are authorized to perform the
required inspections. In Notice 95-5, the FAA required affected
commuters to comply with part 121. No comments were received on this
issue and the final rule is adopted as proposed.

Continuing analysis and surveillance. Section 121.373 on continuing
analysis and surveillance is almost identical to the provisions of
Sec. 135.431. The FAA proposed that affected commuters comply with
Sec. 121.373. Section 121.373 provides for: the establishment by the
certificate holder of a system to continually analyze the performance
and effectiveness of the programs covering maintenance, preventive
maintenance, and alterations; the correction of any deficiencies in
those programs; and the requirement by the Administrator that the
certificate holder make changes in either or both of its programs if
those programs do not contain adequate procedures and standards to meet
the requirements of this part. No comments were received on this issue
and the final rule is adopted as proposed.

Maintenance and preventative maintenance training programs.
Sections 121.375 and 135.433 contain identical requirements prescribing
training programs that ensure that persons performing maintenance or
preventive maintenance functions (including inspection personnel) are
fully informed about procedures, techniques, and new equipment in use
and that those personnel are competent to perform their required
duties. The FAA proposed that operators comply with part 121. On this
issue, no comments were received and the final rule is adopted as
proposed.

Maintenance and preventive maintenance personnel duty time
limitations. Section 121.377 establishes the requirements for
maintenance personnel to be relieved from duty for a period of at least
24 consecutive hours during any 7 consecutive days, or the equivalent
thereof within any calendar month. This requirement is for maintenance
personnel within the United States. This provision would be a new
requirement for affected commuters.

Comments: AACA states that most Alaskan certificate holders utilize
mixed fleets ranging from under 9 passenger seats, 10-19 seats, and
more than 20 seats. These carriers frequently employ maintenance
personnel who are qualified to work on all the aircraft in a particular
certificate holder's fleet, regardless of the aircraft's seating
capacity. If the rule is adopted as proposed, these certificate holders
will have to schedule maintenance personnel according to part 121
standards to avoid inadvertently violating the maintenance personnel
duty time limitations. At locations with limited maintenance personnel
and mixed fleets of 1-to-9, and 10-to-29 seat aircraft, this new
requirement would place an additional administrative scheduling burden
and financial compliance cost on the air carrier. Alternatively, an air
carrier might have to develop and apply two separate work schedules for
mechanics, one for part 121 mechanics and aircraft and another for part
135 mechanics and aircraft. AACA states that the FAA's economic
analysis failed to address any cost impacts of this requirement. AACA
also asks for guidance for those operators who employ maintenance
personnel that might work under both part 121 and part 135.

FAA Response: The existing rule requires only 24 consecutive hours
off during any 7 consecutive days. While it may have been possible to
work mechanics under part 135 7 days a week, without rest, the FAA
believes that the combination of union work rules, Department of Labor
regulations, and general practice of a day of rest each week would, in
effect, accomplish the same result as the rule.

Mechanics must receive adequate rest in order to properly perform
their duties. Prescribing a minimum standard will ensure that some rest
is provided. It would be inconsistent to require rest for the pilots
and flight attendants but not for the people responsible for
maintaining the airplane. The FAA believes that the burden of
scheduling and providing a day of rest would be minimal. Standard time
cards, a common practice, could be used to show compliance.

No FAA regulation prevents a mechanic from working for both a part
121 and a part 135 employer when the mechanic is qualified and, when
working on airplanes operated under part 121, the certificate holder
meets the regulatory requirements of part 121 for time free from duty.

It should also be noted that the rule allows flexibility by
requiring that a certificate holder shall relieve each person
performing maintenance or preventive maintenance from duty for at least
24 consecutive hours during any 7 consecutive days, "or the equivalent
thereof within any calendar month."

The final rule is adopted as proposed.

Certificate Requirements. Sections 121.378 and 135.435 contain
identical requirements specifying that each person, other than a repair
station certificated under the provisions of subpart C of part 145, who
is directly in charge of maintenance, preventive maintenance, or
alterations, and each person performing required inspections, hold an
appropriate airman certificate. The FAA proposed that affected
commuters comply with part 121. No comments were received on this issue
and the final rule is adopted as proposed.

Authority to perform and approve maintenance, preventative
maintenance, and alterations. Sections 121.379 and 135.437 contain
similar requirements allowing certificate holders to perform or make
arrangements with other persons to perform maintenance, preventive
maintenance, and alterations as provided in its continuous
airworthiness maintenance program and its manual. In addition,
a certificate holder may perform these
functions for another certificate holder. The rules require that all
major repairs and alterations must have been accomplished with data
approved by the Administrator. The FAA proposed that affected commuters
comply with part 121. No comments were received on this issue and the
final rule is adopted as proposed.

Maintenance recording requirements. Section 121.380 provides for
the preparation, maintenance, and retention of certain records using
the system specified in the certificate holder's manual. The rule also
specifies the length of time that the records must be retained and
requires that the records be transferred with the airplane at the time
it is sold. A small change was proposed to Sec. 121.380(a)(2) to
accommodate propeller-driven airplanes used by some affected commuters
and to Sec. 121.380(a)(2)(v) to adopt the language found in
Sec. 135.439(a)(2)(v) to provide more complete records on airworthiness
directive compliance.

Comments: Zantop International Airlines, Inc. (a current part 121
certificate holder) objects to the proposed change to
Sec. 121.380(a)(2)(i) that would add engine and propeller total time in
service to the list of items that must be recorded. Zantop says that
the engine and propeller requirement is new for them and that the
aircraft (airframe) total hours in service is the only time transferred
on many of its older aircraft. The new requirement would result in
searching maintenance records to determine the historical time on the
engine and propeller. In some cases this information may not be
available. Zantop recommends that an exemption be provided for older
aircraft or that these records only be required for future
certifications.

FAA Response: Although current Sec. 121.380(a)(2)(i) does not
specifically call for total time in-service records of engines or
propellers, it does require a record of life-limited parts for these
components. The only way to accomplish this is by keeping records for
total time in service. Total time in service records may consist of
aircraft maintenance record pages, separate component cards or pages, a
computer list, or other methods as described in the applicant's manual.

Tracing a life-limited part back to its origin would be required
only in those situations where the certificate holder's records are so
incomplete that an accurate determination of the time elapsed on the
life-limited part could not be made.

The part 135 certificate holders moving to part 121 will have no
impact from this rule, since they are already tracking airframe,
engine, and propeller time under Sec. 135.439(a)(2)(i).

The airframe, engine, and propeller information is helpful in
tracking airworthiness directive compliance and life limits for life-
limited parts. It also standardizes language between part 135 and part
121. The FAA believes that at least some of the current part 121
certificate holders have the information in existing required records
in order to show compliance with life-limited components. However, the
FAA has decided to allow current part 121 operators some time to come
into compliance with the requirements for recording total time for
engines and propellers. The final rule for Sec. 121.380 has been
revised accordingly.

Transfer of maintenance records. Section 121.380a requires the
certificate holder to transfer certain maintenance records to the
purchaser at the time of the sale, either in plain language form or in
coded form. This section is worded the same as Sec. 135.441 except that
the part 121 provision allows the purchaser to select the format of the
transferred records. Notice 95-5 specified that affected commuters
comply with part 121. No comments were received on this issue and the
final rule is adopted as proposed.

VI.A.9. Subpart M--Airman and Crewmember Requirements

Flight attendant complement. Section 121.391 requires one flight
attendant for airplanes having a seating capacity of more than 9 but
less than 51 passengers. Section 135.107 requires one flight attendant
for airplanes having a passenger seating configuration, excluding any
pilot seat, of more than 19 passengers. The FAA retained the
requirement for a flight attendant for more than 9 passengers for
current part 121 airplanes and proposed to amend the section to require
a flight attendant for affected commuters only in airplanes with more
than 19 passenger seats. No comments were received on this issue and
the final rule is adopted as proposed.

Flight attendants being seated during movement on the surface.
Section 121.391(d) states that during movement on the surface, flight
attendants must remain at their duty stations with safety belts and
shoulder harnesses fastened except to perform duties related to the
safety of the airplane and its occupants. Part 135 has a similar
provision in Sec. 135.128(a), except that it does not specify that
flight attendants may be performing safety duties during movement on
the surface. The FAA proposed that affected commuters comply with part
121. On this issue, no comments were received and the final rule is
adopted as proposed.

Flight attendants or other qualified personnel at the gate. The FAA
proposed that all airplanes being operated by affected commuters be
required to comply with current Sec. 121.391(e); that is, they must
have a flight attendant or substitute (such as a flight crewmember or
trained gate agent) on board when the airplane is parked at the gate
and passengers are on board. The substitutes must be given training in
the emergency evacuation procedures for that airplane as required by
Sec. 121.417 and they must be identified to the passengers. If there is
only one flight attendant or other qualified person on board the
airplane, that person must be located in accordance with the
certificate holder's FAA-approved operating procedures.

As a result of the proposed rule, Sec. 121.391(e) applies in the
future to some operations that do not require flight attendants.
Therefore, the FAA proposed to move Sec. 121.391(e) to a new separate
section, proposed Sec. 121.393, to highlight the crewmember
requirements that apply when an airplane is on the ground and
passengers remain on board before continuing to another destination.

Comments: AACA opposes the requirement