| |
 Federal Register Information
 Header Information
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
Amendment 39-1081; AD 70-20-01
Airworthiness Directives; Siai-Marchetti Model 205-22/R Airplanes
PDF Copy (If Available):
Preamble Information
Flap locking mechanism
DATES: Effective September 22, 1970.
Regulatory Information
70-20-01 SIAI-MARCHETTI: Amdt. 39-1081. Applies to Model 205-22/R airplanes.
To prevent malfunction of the flap position locking mechanism, within the next 25 hours' time in service after the effective date of this AD, unless already accomplished, replace the flap system locking pawl (P/N 205-6-052-22) and cup (P/N 205-6-052-23) with a modified locking pawl (P/N 205-6-052-22/A) and modified cup (P/N 205-6-052-23/A) in accordance with SIAI Marchetti Technical Instruction No. 205 I-13, dated 3 April 1970, or an FAA-approved equivalent.
(SIAI Marchetti Service Bulletin No. 205B25 refers to this subject).
This amendment becomes effective September 22, 1970.
Footer Information
Comments
|