| |
AD # | Docket # | Amendment # | Effective Date | Publish Date | Supersedes/ Revises | Superseded By/ Revised By | Current | Title | Subject | Make | MakeInfo | Model | ModelInfo | PartNumber | AFDRType | IssueDate | Attachments | Attachment_Names | Attachment_Lengths |
|---|
| 2009-24-52 | Unknown | | | | 2009-24-51 | |  | Emergency AD: Teledyne Continental Motors (TCM) 240, 360, 470, 520, and 550 series
reciprocating engines | Hydraulic lifters | Teledyne Continental Motors | Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors | Teledyne Continental Motors FSO-470-A,Teledyne Continental Motors GIO-470-A,Teledyne Continental Motors GTSIO-520-C,Teledyne Continental Motors GTSIO-520-D,Teledyne Continental Motors GTSIO-520-E,Teledyne Continental Motors GTSIO-520-F,Teledyne Continental Motors GTSIO-520-H,Teledyne Continental Motors GTSIO-520-K,Teledyne Continental Motors GTSIO-520-L,Teledyne Continental Motors GTSIO-520-M,Teledyne Continental Motors GTSIO-520-N,Teledyne Continental Motors IO-360-A,Teledyne Continental Motors IO-360-AB,Teledyne Continental Motors IO-360-B,Teledyne Continental Motors IO-360-C,Teledyne Continental Motors IO-360-D,Teledyne Continental Motors IO-360-DB,Teledyne Continental Motors IO-360-E,Teledyne Continental Motors IO-360-ES,Teledyne Continental Motors IO-360-G,Teledyne Continental Motors IO-360-GB,Teledyne Continental Motors IO-360-H,Teledyne Continental Motors IO-360-HB,Teledyne Continental Motors IO-360-J,Teledyne Continental Motors IO-360-JB,Teledyne Continental Motors IO-360-K,Teledyne Continental Motors IO-360-KB,Teledyne Continental Motors IO-470-A,Teledyne Continental Motors IO-470-C,Teledyne Continental Motors IO-470-D,Teledyne Continental Motors IO-470-E,Teledyne Continental Motors IO-470-F,Teledyne Continental Motors IO-470-G,Teledyne Continental Motors IO-470-H,Teledyne Continental Motors IO-470-J,Teledyne Continental Motors IO-470-K,Teledyne Continental Motors IO-470-L,Teledyne Continental Motors IO-470-LO,Teledyne Continental Motors IO-470-M,Teledyne Continental Motors IO-470-N,Teledyne Continental Motors IO-470-P,Teledyne Continental Motors IO-470-R,Teledyne Continental Motors IO-470-S,Teledyne Continental Motors IO-470-T,Teledyne Continental Motors IO-470-U,Teledyne Continental Motors IO-470-V,Teledyne Continental Motors IO-470-VO,Teledyne Continental Motors IO-520-A,Teledyne Continental Motors IO-520-B,Teledyne Continental Motors IO-520-BA,Teledyne Continental Motors IO-520-BB,Teledyne Continental Motors IO-520-C,Teledyne Continental Motors IO-520-CB,Teledyne Continental Motors IO-520-D,Teledyne Continental Motors IO-520-E,Teledyne Continental Motors IO-520-F,Teledyne Continental Motors IO-520-J,Teledyne Continental Motors IO-520-K,Teledyne Continental Motors IO-520-L,Teledyne Continental Motors IO-520-M,Teledyne Continental Motors IO-520-MB,Teledyne Continental Motors IO-520-N,Teledyne Continental Motors IO-520-NB,Teledyne Continental Motors IO-550-A,Teledyne Continental Motors IO-550-B,Teledyne Continental Motors IO-550-C,Teledyne Continental Motors IO-550-D,Teledyne Continental Motors IO-550-E,Teledyne Continental Motors IO-550-F,Teledyne Continental Motors IO-550-G,Teledyne Continental Motors IO-550-L,Teledyne Continental Motors IO-550-N,Teledyne Continental Motors IO-550-P,Teledyne Continental Motors IO-550-R,Teledyne Continental Motors IOF-240-B,Teledyne Continental Motors IOF-550-B,Teledyne Continental Motors IOF-550-C,Teledyne Continental Motors IOF-550-D,Teledyne Continental Motors IOF-550-E,Teledyne Continental Motors IOF-550-F,Teledyne Continental Motors IOF-550-L,Teledyne Continental Motors IOF-550-N,Teledyne Continental Motors IOF-550-P,Teledyne Continental Motors IOF-550-R,Teledyne Continental Motors LTSIO-360-E,Teledyne Continental Motors LTSIO-360-EB,Teledyne Continental Motors LTSIO-360-KB,Teledyne Continental Motors LTSIO-360-RB,Teledyne Continental Motors LTSIO-520-AE,Teledyne Continental Motors L/IO-470-A,Teledyne Continental Motors L/IO-520-P,Teledyne Continental Motors O-470-11,Teledyne Continental Motors O-470-11-CI,Teledyne Continental Motors O-470-11B,Teledyne Continental Motors O-470-11B-CI,Teledyne Continental Motors O-470-13,Teledyne Continental Motors O-470-13A,Teledyne Continental Motors O-470-15,Teledyne Continental Motors O-470-2,Teledyne Continental Motors O-470-4,Teledyne Continental Motors O-470-A,Teledyne Continental Motors O-470-B,Teledyne Continental Motors O-470-B-CI,Teledyne Continental Motors O-470-E,Teledyne Continental Motors O-470-G,Teledyne Continental Motors O-470-G-CI,Teledyne Continental Motors O-470-H,Teledyne Continental Motors O-470-J,Teledyne Continental Motors O-470-K,Teledyne Continental Motors O-470-K-CI,Teledyne Continental Motors O-470-L,Teledyne Continental Motors O-470-L-CI,Teledyne Continental Motors O-470-M,Teledyne Continental Motors O-470-M-CI,Teledyne Continental Motors O-470-N,Teledyne Continental Motors O-470-P,Teledyne Continental Motors O-470-R,Teledyne Continental Motors O-470-S,Teledyne Continental Motors O-470-T,Teledyne Continental Motors O-470-U,Teledyne Continental Motors TSIO-360-A,Teledyne Continental Motors TSIO-360-AB,Teledyne Continental Motors TSIO-360-B,Teledyne Continental Motors TSIO-360-BB,Teledyne Continental Motors TSIO-360-C,Teledyne Continental Motors TSIO-360-CB,Teledyne Continental Motors TSIO-360-D,Teledyne Continental Motors TSIO-360-DB,Teledyne Continental Motors TSIO-360-E,Teledyne Continental Motors TSIO-360-EB,Teledyne Continental Motors TSIO-360-F,Teledyne Continental Motors TSIO-360-FB,Teledyne Continental Motors TSIO-360-G,Teledyne Continental Motors TSIO-360-GB,Teledyne Continental Motors TSIO-360-H,Teledyne Continental Motors TSIO-360-HB,Teledyne Continental Motors TSIO-360-JB,Teledyne Continental Motors TSIO-360-KB,Teledyne Continental Motors TSIO-360-LB,Teledyne Continental Motors TSIO-360-MB,Teledyne Continental Motors TSIO-360-NB,Teledyne Continental Motors TSIO-360-PB,Teledyne Continental Motors TSIO-360-RB,Teledyne Continental Motors TSIO-360-SB,Teledyne Continental Motors TSIO-470-B,Teledyne Continental Motors TSIO-470-C,Teledyne Continental Motors TSIO-470-D,Teledyne Continental Motors TSIO-520-A,Teledyne Continental Motors TSIO-520-AE,Teledyne Continental Motors TSIO-520-AF,Teledyne Continental Motors TSIO-520-B,Teledyne Continental Motors TSIO-520-BB,Teledyne Continental Motors TSIO-520-BE,Teledyne Continental Motors TSIO-520-C,Teledyne Continental Motors TSIO-520-CE,Teledyne Continental Motors TSIO-520-D,Teledyne Continental Motors TSIO-520-DB,Teledyne Continental Motors TSIO-520-E,Teledyne Continental Motors TSIO-520-EB,Teledyne Continental Motors TSIO-520-G,Teledyne Continental Motors TSIO-520-H,Teledyne Continental Motors TSIO-520-J,Teledyne Continental Motors TSIO-520-JB,Teledyne Continental Motors TSIO-520-K,Teledyne Continental Motors TSIO-520-KB,Teledyne Continental Motors TSIO-520-L,Teledyne Continental Motors TSIO-520-LB,Teledyne Continental Motors TSIO-520-M,Teledyne Continental Motors TSIO-520-N,Teledyne Continental Motors TSIO-520-NB,Teledyne Continental Motors TSIO-520-P,Teledyne Continental Motors TSIO-520-R,Teledyne Continental Motors TSIO-520-T,Teledyne Continental Motors TSIO-520-U,Teledyne Continental Motors TSIO-520-UB,Teledyne Continental Motors TSIO-520-VB,Teledyne Continental Motors TSIO-520-WB,Teledyne Continental Motors TSIO-550-A,Teledyne Continental Motors TSIO-550-B,Teledyne Continental Motors TSIO-550-C,Teledyne Continental Motors TSIO-550-E,Teledyne Continental Motors TSIO-550-G,Teledyne Continental Motors TSIOF-550-J,Teledyne Continental Motors TSIOL-550-A,Teledyne Continental Motors TSIOL-550-B,Teledyne Continental Motors TSIOL-550-C | FSO-470-A,GIO-470-A,GTSIO-520-C,GTSIO-520-D,GTSIO-520-E,GTSIO-520-F,GTSIO-520-H,GTSIO-520-K,GTSIO-520-L,GTSIO-520-M,GTSIO-520-N,IO-360-A,IO-360-AB,IO-360-B,IO-360-C,IO-360-D,IO-360-DB,IO-360-E,IO-360-ES,IO-360-G,IO-360-GB,IO-360-H,IO-360-HB,IO-360-J,IO-360-JB,IO-360-K,IO-360-KB,IO-470-A,IO-470-C,IO-470-D,IO-470-E,IO-470-F,IO-470-G,IO-470-H,IO-470-J,IO-470-K,IO-470-L,IO-470-LO,IO-470-M,IO-470-N,IO-470-P,IO-470-R,IO-470-S,IO-470-T,IO-470-U,IO-470-V,IO-470-VO,IO-520-A,IO-520-B,IO-520-BA,IO-520-BB,IO-520-C,IO-520-CB,IO-520-D,IO-520-E,IO-520-F,IO-520-J,IO-520-K,IO-520-L,IO-520-M,IO-520-MB,IO-520-N,IO-520-NB,IO-550-A,IO-550-B,IO-550-C,IO-550-D,IO-550-E,IO-550-F,IO-550-G,IO-550-L,IO-550-N,IO-550-P,IO-550-R,IOF-240-B,IOF-550-B,IOF-550-C,IOF-550-D,IOF-550-E,IOF-550-F,IOF-550-L,IOF-550-N,IOF-550-P,IOF-550-R,LTSIO-360-E,LTSIO-360-EB,LTSIO-360-KB,LTSIO-360-RB,LTSIO-520-AE,L/IO-470-A,L/IO-520-P,O-470-11,O-470-11-CI,O-470-11B,O-470-11B-CI,O-470-13,O-470-13A,O-470-15,O-470-2,O-470-4,O-470-A,O-470-B,O-470-B-CI,O-470-E,O-470-G,O-470-G-CI,O-470-H,O-470-J,O-470-K,O-470-K-CI,O-470-L,O-470-L-CI,O-470-M,O-470-M-CI,O-470-N,O-470-P,O-470-R,O-470-S,O-470-T,O-470-U,TSIO-360-A,TSIO-360-AB,TSIO-360-B,TSIO-360-BB,TSIO-360-C,TSIO-360-CB,TSIO-360-D,TSIO-360-DB,TSIO-360-E,TSIO-360-EB,TSIO-360-F,TSIO-360-FB,TSIO-360-G,TSIO-360-GB,TSIO-360-H,TSIO-360-HB,TSIO-360-JB,TSIO-360-KB,TSIO-360-LB,TSIO-360-MB,TSIO-360-NB,TSIO-360-PB,TSIO-360-RB,TSIO-360-SB,TSIO-470-B,TSIO-470-C,TSIO-470-D,TSIO-520-A,TSIO-520-AE,TSIO-520-AF,TSIO-520-B,TSIO-520-BB,TSIO-520-BE,TSIO-520-C,TSIO-520-CE,TSIO-520-D,TSIO-520-DB,TSIO-520-E,TSIO-520-EB,TSIO-520-G,TSIO-520-H,TSIO-520-J,TSIO-520-JB,TSIO-520-K,TSIO-520-KB,TSIO-520-L,TSIO-520-LB,TSIO-520-M,TSIO-520-N,TSIO-520-NB,TSIO-520-P,TSIO-520-R,TSIO-520-T,TSIO-520-U,TSIO-520-UB,TSIO-520-VB,TSIO-520-WB,TSIO-550-A,TSIO-550-B,TSIO-550-C,TSIO-550-E,TSIO-550-G,TSIOF-550-J,TSIOL-550-A,TSIOL-550-B,TSIOL-550-C | Part 39 | Emergency AD | 11/18/2009 | 1 | 2009-24-52_Emergency.pdf | 24160 |
| 2009-24-51 | Unknown | | | | | 2009-24-52 | | Emergency AD: Teledyne Continental Motors (TCM) 240, 360, 470, and 520 series reciprocating
engines | Hydraulic lifters | Teledyne Continental Motors | Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors | Teledyne Continental Motors FSO-470-A,Teledyne Continental Motors GIO-470-A,Teledyne Continental Motors GTSIO-520-C,Teledyne Continental Motors GTSIO-520-D,Teledyne Continental Motors GTSIO-520-E,Teledyne Continental Motors GTSIO-520-F,Teledyne Continental Motors GTSIO-520-H,Teledyne Continental Motors GTSIO-520-K,Teledyne Continental Motors GTSIO-520-L,Teledyne Continental Motors GTSIO-520-M,Teledyne Continental Motors GTSIO-520-N,Teledyne Continental Motors IO-240-A,Teledyne Continental Motors IO-240-B,Teledyne Continental Motors IO-360-A,Teledyne Continental Motors IO-360-AB,Teledyne Continental Motors IO-360-B,Teledyne Continental Motors IO-360-C,Teledyne Continental Motors IO-360-D,Teledyne Continental Motors IO-360-DB,Teledyne Continental Motors IO-360-E,Teledyne Continental Motors IO-360-ES,Teledyne Continental Motors IO-360-G,Teledyne Continental Motors IO-360-GB,Teledyne Continental Motors IO-360-H,Teledyne Continental Motors IO-360-HB,Teledyne Continental Motors IO-360-J,Teledyne Continental Motors IO-360-JB,Teledyne Continental Motors IO-360-K,Teledyne Continental Motors IO-360-KB,Teledyne Continental Motors IO-470-A,Teledyne Continental Motors IO-470-C,Teledyne Continental Motors IO-470-D,Teledyne Continental Motors IO-470-E,Teledyne Continental Motors IO-470-F,Teledyne Continental Motors IO-470-G,Teledyne Continental Motors IO-470-H,Teledyne Continental Motors IO-470-J,Teledyne Continental Motors IO-470-K,Teledyne Continental Motors IO-470-L,Teledyne Continental Motors IO-470-LO,Teledyne Continental Motors IO-470-M,Teledyne Continental Motors IO-470-N,Teledyne Continental Motors IO-470-P,Teledyne Continental Motors IO-470-R,Teledyne Continental Motors IO-470-S,Teledyne Continental Motors IO-470-T,Teledyne Continental Motors IO-470-U,Teledyne Continental Motors IO-470-V,Teledyne Continental Motors IO-470-VO,Teledyne Continental Motors IO-520-A,Teledyne Continental Motors IO-520-B,Teledyne Continental Motors IO-520-BA,Teledyne Continental Motors IO-520-BB,Teledyne Continental Motors IO-520-C,Teledyne Continental Motors IO-520-CB,Teledyne Continental Motors IO-520-D,Teledyne Continental Motors IO-520-E,Teledyne Continental Motors IO-520-F,Teledyne Continental Motors IO-520-J,Teledyne Continental Motors IO-520-K,Teledyne Continental Motors IO-520-L,Teledyne Continental Motors IO-520-M,Teledyne Continental Motors IO-520-MB,Teledyne Continental Motors IO-520-N,Teledyne Continental Motors IO-520-NB,Teledyne Continental Motors IOF-240-B,Teledyne Continental Motors LTSIO-360-E,Teledyne Continental Motors LTSIO-360-EB,Teledyne Continental Motors LTSIO-360-KB,Teledyne Continental Motors LTSIO-360-RB,Teledyne Continental Motors LTSIO-520-AE,Teledyne Continental Motors L/IO-470-A,Teledyne Continental Motors L/IO-520-P,Teledyne Continental Motors O-470-11,Teledyne Continental Motors O-470-11-CI,Teledyne Continental Motors O-470-11B,Teledyne Continental Motors O-470-11B-CI,Teledyne Continental Motors O-470-13,Teledyne Continental Motors O-470-13A,Teledyne Continental Motors O-470-15,Teledyne Continental Motors O-470-2,Teledyne Continental Motors O-470-4,Teledyne Continental Motors O-470-A,Teledyne Continental Motors O-470-B,Teledyne Continental Motors O-470-B-CI,Teledyne Continental Motors O-470-E,Teledyne Continental Motors O-470-G,Teledyne Continental Motors O-470-G-CI,Teledyne Continental Motors O-470-H,Teledyne Continental Motors O-470-J,Teledyne Continental Motors O-470-K,Teledyne Continental Motors O-470-K-CI,Teledyne Continental Motors O-470-L,Teledyne Continental Motors O-470-L-CI,Teledyne Continental Motors O-470-M,Teledyne Continental Motors O-470-M-CI,Teledyne Continental Motors O-470-N,Teledyne Continental Motors O-470-P,Teledyne Continental Motors O-470-R,Teledyne Continental Motors O-470-S,Teledyne Continental Motors O-470-T,Teledyne Continental Motors O-470-U,Teledyne Continental Motors TSIO-360-A,Teledyne Continental Motors TSIO-360-AB,Teledyne Continental Motors TSIO-360-B,Teledyne Continental Motors TSIO-360-BB,Teledyne Continental Motors TSIO-360-C,Teledyne Continental Motors TSIO-360-CB,Teledyne Continental Motors TSIO-360-D,Teledyne Continental Motors TSIO-360-DB,Teledyne Continental Motors TSIO-360-E,Teledyne Continental Motors TSIO-360-EB,Teledyne Continental Motors TSIO-360-F,Teledyne Continental Motors TSIO-360-FB,Teledyne Continental Motors TSIO-360-G,Teledyne Continental Motors TSIO-360-GB,Teledyne Continental Motors TSIO-360-H,Teledyne Continental Motors TSIO-360-HB,Teledyne Continental Motors TSIO-360-JB,Teledyne Continental Motors TSIO-360-KB,Teledyne Continental Motors TSIO-360-LB,Teledyne Continental Motors TSIO-360-MB,Teledyne Continental Motors TSIO-360-NB,Teledyne Continental Motors TSIO-360-PB,Teledyne Continental Motors TSIO-360-RB,Teledyne Continental Motors TSIO-360-SB,Teledyne Continental Motors TSIO-470-B,Teledyne Continental Motors TSIO-470-C,Teledyne Continental Motors TSIO-470-D,Teledyne Continental Motors TSIO-520-A,Teledyne Continental Motors TSIO-520-AE,Teledyne Continental Motors TSIO-520-AF,Teledyne Continental Motors TSIO-520-B,Teledyne Continental Motors TSIO-520-BB,Teledyne Continental Motors TSIO-520-BE,Teledyne Continental Motors TSIO-520-C,Teledyne Continental Motors TSIO-520-CE,Teledyne Continental Motors TSIO-520-D,Teledyne Continental Motors TSIO-520-DB,Teledyne Continental Motors TSIO-520-E,Teledyne Continental Motors TSIO-520-EB,Teledyne Continental Motors TSIO-520-G,Teledyne Continental Motors TSIO-520-H,Teledyne Continental Motors TSIO-520-J,Teledyne Continental Motors TSIO-520-JB,Teledyne Continental Motors TSIO-520-K,Teledyne Continental Motors TSIO-520-KB,Teledyne Continental Motors TSIO-520-L,Teledyne Continental Motors TSIO-520-LB,Teledyne Continental Motors TSIO-520-M,Teledyne Continental Motors TSIO-520-N,Teledyne Continental Motors TSIO-520-NB,Teledyne Continental Motors TSIO-520-P,Teledyne Continental Motors TSIO-520-R,Teledyne Continental Motors TSIO-520-T,Teledyne Continental Motors TSIO-520-U,Teledyne Continental Motors TSIO-520-UB,Teledyne Continental Motors TSIO-520-VB,Teledyne Continental Motors TSIO-520-WB | FSO-470-A,GIO-470-A,GTSIO-520-C,GTSIO-520-D,GTSIO-520-E,GTSIO-520-F,GTSIO-520-H,GTSIO-520-K,GTSIO-520-L,GTSIO-520-M,GTSIO-520-N,IO-240-A,IO-240-B,IO-360-A,IO-360-AB,IO-360-B,IO-360-C,IO-360-D,IO-360-DB,IO-360-E,IO-360-ES,IO-360-G,IO-360-GB,IO-360-H,IO-360-HB,IO-360-J,IO-360-JB,IO-360-K,IO-360-KB,IO-470-A,IO-470-C,IO-470-D,IO-470-E,IO-470-F,IO-470-G,IO-470-H,IO-470-J,IO-470-K,IO-470-L,IO-470-LO,IO-470-M,IO-470-N,IO-470-P,IO-470-R,IO-470-S,IO-470-T,IO-470-U,IO-470-V,IO-470-VO,IO-520-A,IO-520-B,IO-520-BA,IO-520-BB,IO-520-C,IO-520-CB,IO-520-D,IO-520-E,IO-520-F,IO-520-J,IO-520-K,IO-520-L,IO-520-M,IO-520-MB,IO-520-N,IO-520-NB,IOF-240-B,LTSIO-360-E,LTSIO-360-EB,LTSIO-360-KB,LTSIO-360-RB,LTSIO-520-AE,L/IO-470-A,L/IO-520-P,O-470-11,O-470-11-CI,O-470-11B,O-470-11B-CI,O-470-13,O-470-13A,O-470-15,O-470-2,O-470-4,O-470-A,O-470-B,O-470-B-CI,O-470-E,O-470-G,O-470-G-CI,O-470-H,O-470-J,O-470-K,O-470-K-CI,O-470-L,O-470-L-CI,O-470-M,O-470-M-CI,O-470-N,O-470-P,O-470-R,O-470-S,O-470-T,O-470-U,TSIO-360-A,TSIO-360-AB,TSIO-360-B,TSIO-360-BB,TSIO-360-C,TSIO-360-CB,TSIO-360-D,TSIO-360-DB,TSIO-360-E,TSIO-360-EB,TSIO-360-F,TSIO-360-FB,TSIO-360-G,TSIO-360-GB,TSIO-360-H,TSIO-360-HB,TSIO-360-JB,TSIO-360-KB,TSIO-360-LB,TSIO-360-MB,TSIO-360-NB,TSIO-360-PB,TSIO-360-RB,TSIO-360-SB,TSIO-470-B,TSIO-470-C,TSIO-470-D,TSIO-520-A,TSIO-520-AE,TSIO-520-AF,TSIO-520-B,TSIO-520-BB,TSIO-520-BE,TSIO-520-C,TSIO-520-CE,TSIO-520-D,TSIO-520-DB,TSIO-520-E,TSIO-520-EB,TSIO-520-G,TSIO-520-H,TSIO-520-J,TSIO-520-JB,TSIO-520-K,TSIO-520-KB,TSIO-520-L,TSIO-520-LB,TSIO-520-M,TSIO-520-N,TSIO-520-NB,TSIO-520-P,TSIO-520-R,TSIO-520-T,TSIO-520-U,TSIO-520-UB,TSIO-520-VB,TSIO-520-WB | Part 39 | Emergency AD | 11/16/2009 | 1 | 2009-24-51_Emergency.pdf | 23932 |
| 2009-23-51 | Unknown | | | | | | | Emergency AD: Sikorsky Model S-92A helicopters | Main gearbox | Sikorsky Aircraft Corporation | Sikorsky Aircraft Corporation | Sikorsky Aircraft Corporation S-92A | S-92A | Part 39 | Emergency AD | 10/29/2009 | 1 | 2009-23-51_Emergency.pdf | 22013 |
| 2009-23-12 | FAA-2009-0557 | 39-16086 | 06/19/2009 | 11/13/2009 | | | | SOCATA Model TBM 700 Airplanes | Oxygen | SOCATA | SOCATA | SOCATA TBM 700 | TBM 700 | Part 39 | Airworthiness Directives | 11/06/2009 | 1 | 2009-23-12.pdf | 32046 |
| 2009-23-11 | FAA-2009-1039 | 39-16085 | 12/02/2009 | 11/12/2009 | | | | Empresa Brasileira de Aeronautica S.A. (EMBRAER)
Model EMB-500 Airplanes | Ice and Rain Protection | Embraer - Empresa Brasileira de Aeronautica S.A. | Embraer - Empresa Brasileira de Aer | Embraer - Empresa Brasileira de Aeronautica S.A. EMB-500 | EMB-500 | Part 39 | Airworthiness Directives | 11/02/2009 | 1 | 2009-23-11.pdf | 253934 |
| 2009-23-10 | FAA-2009-1026 | 39-16084 | 11/24/2009 | 11/09/2009 | 2008-15-05 | | | Boeing Model 737-300, -400, and -500 Series Airplanes | Wings | Boeing Company^ The | Boeing Company, The,Boeing Company, The,Boeing Company, The | Boeing Company^ The 737-300 Series,Boeing Company^ The 737-400 Series,Boeing Company^ The 737-500 Series | 737-300 Series,737-400 Series,737-500 Series | Part 39 | Airworthiness Directives | 10/26/2009 | 1 | 2009-23-10.pdf | 41557 |
| 2009-23-09 | FAA-2009-0689 | 39-16081 | 12/14/2009 | 11/09/2009 | | | | Bombardier Model CL-600-1A11 (CL-600), CL-600-2A12
(CL-601), CL-600-2B16 (CL-601-3A) Airplanes | Electrical power
| Bombardier Inc. | Bombardier Inc.,Bombardier Inc.,Bombardier Inc. | Bombardier Inc. CL-600-1A11 (CL-600),Bombardier Inc. CL-600-2A12 (CL-601),Bombardier Inc. CL-600-2B16 (CL-601-3A) | CL-600-1A11 (CL-600),CL-600-2A12 (CL-601),CL-600-2B16 (CL-601-3A) | Part 39 | Airworthiness Directives | 11/06/2009 | 1 | 2009-23-09.pdf | 32850 |
| 2009-23-08 | FAA-2009-0687 | 39-16080 | 12/17/2009 | 11/12/2009 | 2007-06-53 | | | Empresa Brasileira de Aeronautica S.A. (EMBRAER)
Model ERJ 170 and ERJ 190 Airplanes | Doors
| Embraer - Empresa Brasileira de Aeronautica S.A. | Embraer - Empresa Brasileira de Aer,Embraer - Empresa Brasileira de Aer,Embraer - Empresa Brasileira de Aer,Embraer - Empresa Brasileira de Aer,Embraer - Empresa Brasileira de Aer,Embraer - Empresa Brasileira de Aer,Embraer - Empresa Brasileira de Aer,Embraer - Empresa Brasileira de Aer,Embraer - Empresa Brasileira de Aer,Embraer - Empresa Brasileira de Aer,Embraer - Empresa Brasileira de Aer,Embraer - Empresa Brasileira de Aer,Embraer - Empresa Brasileira de Aer | Embraer - Empresa Brasileira de Aeronautica S.A. ERJ 170-100 LR,Embraer - Empresa Brasileira de Aeronautica S.A. ERJ 170-100 SE,Embraer - Empresa Brasileira de Aeronautica S.A. ERJ 170-100 STD,Embraer - Empresa Brasileira de Aeronautica S.A. ERJ 170-100 SU,Embraer - Empresa Brasileira de Aeronautica S.A. ERJ 170-200 LR,Embraer - Empresa Brasileira de Aeronautica S.A. ERJ 170-200 STD,Embraer - Empresa Brasileira de Aeronautica S.A. ERJ 170-200 SU,Embraer - Empresa Brasileira de Aeronautica S.A. ERJ 190-100 IGW,Embraer - Empresa Brasileira de Aeronautica S.A. ERJ 190-100 LR,Embraer - Empresa Brasileira de Aeronautica S.A. ERJ 190-100 STD,Embraer - Empresa Brasileira de Aeronautica S.A. ERJ 190-200 IGW,Embraer - Empresa Brasileira de Aeronautica S.A. ERJ 190-200 LR,Embraer - Empresa Brasileira de Aeronautica S.A. ERJ 190-200 STD | ERJ 170-100 LR,ERJ 170-100 SE,ERJ 170-100 STD,ERJ 170-100 SU,ERJ 170-200 LR,ERJ 170-200 STD,ERJ 170-200 SU,ERJ 190-100 IGW,ERJ 190-100 LR,ERJ 190-100 STD,ERJ 190-200 IGW,ERJ 190-200 LR,ERJ 190-200 STD | Part 39 | Airworthiness Directives | 10/26/2009 | 1 | 2009-23-08.pdf | 43719 |
| 2009-23-07 | FAA-2009-0134 | 39-16079 | 12/14/2009 | 11/09/2009 | | | | Saab AB, Saab Aerosystems Model SAAB 340A
(SAAB/SF340A) and SAAB 340B Airplanes | Hydraulic power | Saab AB^ Saab Aerosystems | Saab AB, Saab Aerosystems,Saab AB, Saab Aerosystems | Saab AB^ Saab Aerosystems 340A (SAAB SF340A),Saab AB^ Saab Aerosystems SAAB 340B | 340A (SAAB SF340A),SAAB 340B | Part 39 | Airworthiness Directives | 10/26/2009 | 1 | 2009-23-07.pdf | 34810 |
| 2009-23-05 | FAA-2008-1215 | 39-16077 | 12/14/2009 | 11/09/2009 | | | | Airbus Model A318-111, -112, A319, A320, and A321
Series Airplanes | Instruments | Airbus | Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus | Airbus A318 Model -111,Airbus A318 Model -112,Airbus A319 Model -111,Airbus A319 Model -112,Airbus A319 Model -113,Airbus A319 Model -114,Airbus A319 Model -115,Airbus A319 Model -131,Airbus A319 Model -132,Airbus A319 Model -133,Airbus A320 Model -111,Airbus A320 Model -211,Airbus A320 Model -212,Airbus A320 Model -214,Airbus A320 Model -231,Airbus A320 Model -232,Airbus A320 Model -233,Airbus A321 Model-212,Airbus A321 Model-213,Airbus A321 Model-232,Airbus A321 Model -111,Airbus A321 Model -112,Airbus A321 Model -131,Airbus A321 Model -211,Airbus A321 Model -231 | A318 Model -111,A318 Model -112,A319 Model -111,A319 Model -112,A319 Model -113,A319 Model -114,A319 Model -115,A319 Model -131,A319 Model -132,A319 Model -133,A320 Model -111,A320 Model -211,A320 Model -212,A320 Model -214,A320 Model -231,A320 Model -232,A320 Model -233,A321 Model-212,A321 Model-213,A321 Model-232,A321 Model -111,A321 Model -112,A321 Model -131,A321 Model -211,A321 Model -231 | Part 39 | Airworthiness Directives | 10/26/2009 | 1 | 2009-23-05.pdf | 34613 |
| 2009-23-04 | FAA-2007-28281 | 39-16076 | 12/14/2009 | 11/09/2009 | | | | Boeing Model 767 Airplanes | Fuel tank | Boeing Company^ The | Boeing Company, The,Boeing Company, The,Boeing Company, The,Boeing Company, The | Boeing Company^ The 767-200 Series,Boeing Company^ The 767-300 Series,Boeing Company^ The 767-300F Series,Boeing Company^ The 767-400ER Series | 767-200 Series,767-300 Series,767-300F Series,767-400ER Series | Part 39 | Airworthiness Directives | 10/26/2009 | 1 | 2009-23-04.pdf | 44104 |
| 2009-23-03 | FAA-2009-0165 | 39-16075 | 12/14/2009 | 11/09/2009 | 2006-24-11 | | | Hawker Beechcraft Corporation (Type Certificate
Previously Held by Raytheon Aircraft Company) Models 1900, 1900C, and 1900D
Airplanes | Flanges | Hawker Beechcraft Corporation | Hawker Beechcraft Corporation,Hawker Beechcraft Corporation,Hawker Beechcraft Corporation,Hawker Beechcraft Corporation | Hawker Beechcraft Corporation 1900,Hawker Beechcraft Corporation 1900C,Hawker Beechcraft Corporation 1900C (C-12J),Hawker Beechcraft Corporation 1900D | 1900,1900C,1900C (C-12J),1900D | Part 39 | Airworthiness Directives | 10/27/2009 | 1 | 2009-23-03.pdf | 39774 |
| 2009-23-02 | FAA-2009-0310 | 39-16073 | 12/14/2009 | 11/09/2009 | | | | Bombardier Model CL-600-2B19 (Regional Jet Series 100
& 440) Airplanes | Flight Controls | Bombardier Inc. | Bombardier Inc.,Bombardier Inc. | Bombardier Inc. CL-600-2B19 (Regional Jet Series 100),Bombardier Inc. CL-600-2B19 (Regional Jet Series 440) | CL-600-2B19 (Regional Jet Series 100),CL-600-2B19 (Regional Jet Series 440) | Part 39 | Airworthiness Directives | 10/19/2009 | 1 | 2009-23-02.pdf | 36434 |
| 2009-23-01 | FAA-2008-1312 | 39-16072 | 12/08/2009 | 11/03/2009 | | | | Hawker Beechcraft Corporation Model 1900, 1900C, and
1900D Airplanes | Main Landing Gear | Hawker Beechcraft Corporation | Hawker Beechcraft Corporation,Hawker Beechcraft Corporation,Hawker Beechcraft Corporation | Hawker Beechcraft Corporation 1900,Hawker Beechcraft Corporation 1900C,Hawker Beechcraft Corporation 1900D | 1900,1900C,1900D | Part 39 | Airworthiness Directives | 10/23/2009 | 1 | 2009-23-01.pdf | 36700 |
| 2009-22-14 | FAA-2008-1362 | 39-16067 | 12/08/2009 | 11/03/2009 | | | | Boeing Model 747-200C and 747-200F Series Airplanes | Main equipment center | Boeing Company^ The | Boeing Company, The,Boeing Company, The | Boeing Company^ The 747-200C Series,Boeing Company^ The 747-200F Series | 747-200C Series,747-200F Series | Part 39 | Airworthiness Directives | 10/19/2009 | 1 | 2009-22-14.pdf | 32612 |
| 2009-22-13 | FAA-2009-0314 | 39-16066 | 12/03/2009 | 10/29/2009 | | | | Boeing Model 767-200, -300, -300F, and -400ER Series
Airplanes | Fuel | Boeing Company^ The | Boeing Company, The,Boeing Company, The,Boeing Company, The,Boeing Company, The | Boeing Company^ The 767-200 Series,Boeing Company^ The 767-300 Series,Boeing Company^ The 767-300F Series,Boeing Company^ The 767-400ER Series | 767-200 Series,767-300 Series,767-300F Series,767-400ER Series | Part 39 | Airworthiness Directives | 10/19/2009 | 1 | 2009-22-13.pdf | 31778 |
| 2009-22-12 | FAA-2009-0998 | 39-16065 | 11/13/2009 | 10/29/2009 | | | | Bombardier Model CL-600-2C10 (Regional Jet Series
700, 701 & 702) Airplanes, Model CL-600-2D15 (Regional Jet Series 705)
Airplanes, and Model CL-600-2D24 (Regional Jet Series 900) Airplanes | Flight Controls
| Bombardier Inc. | Bombardier Inc.,Bombardier Inc.,Bombardier Inc.,Bombardier Inc.,Bombardier Inc. | Bombardier Inc. CL-600-2C10 (Regional Jet Series 700),Bombardier Inc. CL-600-2C10 (Regional Jet Series 701),Bombardier Inc. CL-600-2C10 (Regional Jet Series 702),Bombardier Inc. CL-600-2D15 (Regional Jet Series 705),Bombardier Inc. CL-600-2D24 (Regional Jet Series 900) | CL-600-2C10 (Regional Jet Series 700),CL-600-2C10 (Regional Jet Series 701),CL-600-2C10 (Regional Jet Series 702),CL-600-2D15 (Regional Jet Series 705),CL-600-2D24 (Regional Jet Series 900) | Part 39 | Airworthiness Directives | 10/16/2009 | 1 | 2009-22-12.pdf | 36946 |
| 2009-22-11 | FAA-2009-1003 | 39-16064 | 11/16/2009 | 10/30/2009 | | | | Bell Helicopter Textron Canada Model 407 and 427
Helicopters | Swashplate link assembly bearing
| Bell Helicopter Textron (Canada) | Bell Helicopter Textron (Canada),Bell Helicopter Textron (Canada) | Bell Helicopter Textron (Canada) 407,Bell Helicopter Textron (Canada) 427 | 407,427 | Part 39 | Airworthiness Directives | 10/20/2009 | 1 | 2009-22-11.pdf | 32088 |
| 2009-22-09 | FAA-2009-0399 | 39-16060 | 12/03/2009 | 10/29/2009 | | | | Bombardier Model CL-600-2C10 (Regional Jet Series
700, 701 & 702), CL-600-2D15 (Regional Jet Series 705), and CL-600-2D24
(Regional Jet Series 900) Airplanes | Airborne Auxiliary Power
| Bombardier Inc. | Bombardier Inc.,Bombardier Inc.,Bombardier Inc.,Bombardier Inc.,Bombardier Inc. | Bombardier Inc. CL-600-2C10 (Regional Jet Series 700),Bombardier Inc. CL-600-2C10 (Regional Jet Series 701),Bombardier Inc. CL-600-2C10 (Regional Jet Series 702),Bombardier Inc. CL-600-2D15 (Regional Jet Series 705),Bombardier Inc. CL-600-2D24 (Regional Jet Series 900) | CL-600-2C10 (Regional Jet Series 700),CL-600-2C10 (Regional Jet Series 701),CL-600-2C10 (Regional Jet Series 702),CL-600-2D15 (Regional Jet Series 705),CL-600-2D24 (Regional Jet Series 900) | Part 39 | Airworthiness Directives | 10/19/2009 | 1 | 2009-22-09.pdf | 33690 |
| 2009-22-08 | FAA-2008-1326 | 39-16059 | 12/03/2009 | 10/29/2009 | | | | Boeing Model 747 Airplanes; and Boeing Model 757-200,
-200PF, and -300 Series Airplanes | Control switches
| Boeing Company^ The | Boeing Company, The,Boeing Company, The,Boeing Company, The,Boeing Company, The,Boeing Company, The,Boeing Company, The,Boeing Company, The,Boeing Company, The,Boeing Company, The,Boeing Company, The,Boeing Company, The,Boeing Company, The,Boeing Company, The,Boeing Company, The,Boeing Company, The | Boeing Company^ The 747-100 Series,Boeing Company^ The 747-100B Series,Boeing Company^ The 747-100B SUD Series,Boeing Company^ The 747-200B Series,Boeing Company^ The 747-200C Series,Boeing Company^ The 747-200F Series,Boeing Company^ The 747-300 Series,Boeing Company^ The 747-400 Series,Boeing Company^ The 747-400D Series,Boeing Company^ The 747-400F Series,Boeing Company^ The 747SP Series,Boeing Company^ The 747SR Series,Boeing Company^ The 757-200 Series,Boeing Company^ The 757-200PF Series,Boeing Company^ The 757-300 Series | 747-100 Series,747-100B Series,747-100B SUD Series,747-200B Series,747-200C Series,747-200F Series,747-300 Series,747-400 Series,747-400D Series,747-400F Series,747SP Series,747SR Series,757-200 Series,757-200PF Series,757-300 Series | Part 39 | Airworthiness Directives | 10/19/2009 | 1 | 2009-22-08.pdf | 33992 |
| 2009-22-07 | FAA-2009-0654 | 39-16058 | 12/03/2009 | 10/29/2009 | | | | Saab AB, Saab Aerosystems Model SAAB 2000 Airplanes | Engine oil. | Saab AB^ Saab Aerosystems | Saab AB, Saab Aerosystems | Saab AB^ Saab Aerosystems SAAB 2000 | SAAB 2000 | Part 39 | Airworthiness Directives | 10/19/2009 | 1 | 2009-22-07.pdf | 32526 |
| 2009-22-06 | FAA-2009-0294 | 39-16057 | 11/30/2009 | 10/26/2009 | | | | International Aero Engines AG (IAE) V2500-A1,
V2527E-A5, V2530-A5, and V2528-D5 Turbofan Engines | HPC stage 9-12 disc assembly | International Aero Engines AG (IAE) | International Aero Engines AG (IAE),International Aero Engines AG (IAE),International Aero Engines AG (IAE),International Aero Engines AG (IAE) | International Aero Engines AG (IAE) V2500-A1,International Aero Engines AG (IAE) V2527E-A5,International Aero Engines AG (IAE) V2528-D5,International Aero Engines AG (IAE) V2530-A5 | V2500-A1,V2527E-A5,V2528-D5,V2530-A5 | Part 39 | Airworthiness Directives | 10/16/2009 | 1 | 2009-22-06.pdf | 29152 |
| 2009-22-04 | FAA-2009-0952 | 39-16055 | 11/12/2009 | 10/28/2009 | | | | Eurocopter France (ECF) Model EC 155B and EC155B1
Helicopters | Freezing of the route display on the navigation display (ND) in the Sector mode
| Eurocopter France | Eurocopter France,Eurocopter France | Eurocopter France EC 155B,Eurocopter France EC155B1 | EC 155B,EC155B1 | Part 39 | Airworthiness Directives | 09/16/2009 | 1 | 2009-22-04.pdf | 31842 |
| 2009-22-03 | FAA-2006-25244 | 39-16054 | 11/12/2009 | 10/27/2009 | 2006-18-15 | | | Hartzell Propeller Inc. ()HC-()2Y(K,R)- () Series
Propellers | Propeller hub
| Hartzell Propeller^ Inc. | Hartzell Propeller, Inc.,Hartzell Propeller, Inc.,Hartzell Propeller, Inc.,Hartzell Propeller, Inc.,Hartzell Propeller, Inc.,Hartzell Propeller, Inc.,Hartzell Propeller, Inc.,Hartzell Propeller, Inc. | Hartzell Propeller^ Inc. DHC-E2Y,Hartzell Propeller^ Inc. HC-C2Y,Hartzell Propeller^ Inc. HC-E2Y,Hartzell Propeller^ Inc. HC-F2YR-1,Hartzell Propeller^ Inc. HC-F2YR-2,Hartzell Propeller^ Inc. HC-I2YR-1,Hartzell Propeller^ Inc. HC-M2YR-1,Hartzell Propeller^ Inc. HC-M2YR-2 | DHC-E2Y,HC-C2Y,HC-E2Y,HC-F2YR-1,HC-F2YR-2,HC-I2YR-1,HC-M2YR-1,HC-M2YR-2 | Part 39 | Airworthiness Directives | 10/02/2009 | 1 | 2009-22-03.pdf | 53515 |
| 2009-22-02 | FAA-2009-0745 | 39-16053 | 12/03/2009 | 10/29/2009 | | | | American Champion Aircraft Corp. Models 7ECA, 7GCAA,
7GCBC, 7KCAB, 8KCAB, and 8GCBC Airplanes | Rear seat back hinge area and excessive elongation of the rear seat hinge bolt hole
| American Champion Aircraft Corp. | American Champion Aircraft Corp.,American Champion Aircraft Corp.,American Champion Aircraft Corp.,American Champion Aircraft Corp.,American Champion Aircraft Corp.,American Champion Aircraft Corp. | American Champion Aircraft Corp. 7ECA,American Champion Aircraft Corp. 7GCAA,American Champion Aircraft Corp. 7GCBC,American Champion Aircraft Corp. 7KCAB,American Champion Aircraft Corp. 8GCBC,American Champion Aircraft Corp. 8KCAB | 7ECA,7GCAA,7GCBC,7KCAB,8GCBC,8KCAB | Part 39 | Airworthiness Directives | 10/13/2009 | 1 | 2009-22-02.pdf | 30540 |
| 2009-22-01 | FAA-2007-0037 | 39-16052 | 11/12/2009 | 10/27/2009 | 2008-10-14 | | | Rolls-Royce Deutschland Ltd. & Co. KG. (RRD) Tay
650-15 Turbofan Engines | Low-pressure turbine disk stage 2 or stage 3 | Rolls-Royce Deutschland Ltd & Co KG | Rolls-Royce Deutschland Ltd & Co KG | Rolls-Royce Deutschland Ltd & Co KG TAY 650-15 | TAY 650-15 | Part 39 | Airworthiness Directives | 10/08/2009 | 1 | 2009-22-01.pdf | 35778 |
| 2009-21-12 | FAA-2008-0979 | 39-16051 | 12/01/2009 | 10/27/2009 | | | | Airbus Model A300-600 Airplanes | Flight controls.
| Airbus | Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus | Airbus A300^ Model B4-601,Airbus A300^ Model B4-603,Airbus A300^ Model B4-605R,Airbus A300^ Model B4-620,Airbus A300^ Model B4-622,Airbus A300^ Model B4-622R,Airbus A300^ Model C4-605R Variant F,Airbus A300^ Model F4-605R,Airbus A300^ Model F4-622R | A300, Model B4-601,A300, Model B4-603,A300, Model B4-605R,A300, Model B4-620,A300, Model B4-622,A300, Model B4-622R,A300, Model C4-605R Variant F,A300, Model F4-605R,A300, Model F4-622R | Part 39 | Airworthiness Directives | 10/07/2009 | 1 | 2009-21-12.pdf | 46412 |
| 2009-21-11 | FAA-2009-0348 | 39-16050 | 11/20/2009 | 10/16/2009 | | | | Turbomeca S.A. ARRIUS 1A Turboshaft Engines | Cycle life limit value for ARRIUS 1A balancing piston.
| Turbomeca S.A. | Turbomeca S.A. | Turbomeca S.A. Arrius 1A | Arrius 1A | Part 39 | Airworthiness Directives | 10/08/2009 | 1 | 2009-21-11.pdf | 28878 |
| 2009-21-09 | FAA-2009-1369 | 39-16048 | 11/20/2009 | 10/16/2009 | 2003-15-06 | | | Rolls-Royce plc RB211 Trent 800 Series Turbofan
Engines | High-pressure (HP) compressor rotor rear stage 5 and 6 discs and cone shafts | Rolls-Royce plc | Rolls-Royce plc,Rolls-Royce plc,Rolls-Royce plc,Rolls-Royce plc,Rolls-Royce plc,Rolls-Royce plc | Rolls-Royce plc RB211-Trent-892B-17,Rolls-Royce plc RB211-Trent-895-17,Rolls-Royce plc RB211-Trent 875-17,Rolls-Royce plc RB211-Trent 877-17,Rolls-Royce plc RB211-Trent 884-17,Rolls-Royce plc RB211-Trent 892-17 | RB211-Trent-892B-17,RB211-Trent-895-17,RB211-Trent 875-17,RB211-Trent 877-17,RB211-Trent 884-17,RB211-Trent 892-17 | Part 39 | Airworthiness Directives | 10/08/2009 | 1 | 2009-21-09.pdf | 28949 |
| 2009-21-08 | FAA-2009-0699 | 39-16047 | 12/14/2009 | 11/09/2009 | | | | PIAGGIO AERO INDUSTRIES S.p.A Model PIAGGIO P-180
Airplanes | Landing Gear
| Piaggio Aero Industries S.p.A. | Piaggio Aero Industries S.p.A. | Piaggio Aero Industries S.p.A. P-180 | P-180 | Part 39 | Airworthiness Directives | 10/07/2009 | 1 | 2009-21-08.pdf | 35980 |
| 2009-21-07 | FAA-2009-0018 | 39-16044 | 12/01/2009 | 10/27/2009 | | | | General Electric Company CF6-80C2 Series Turbofan
Engines | Thrust and thrust control
| General Electric Company | General Electric Company,General Electric Company,General Electric Company,General Electric Company,General Electric Company,General Electric Company,General Electric Company,General Electric Company,General Electric Company,General Electric Company,General Electric Company,General Electric Company,General Electric Company,General Electric Company,General Electric Company,General Electric Company,General Electric Company,General Electric Company,General Electric Company,General Electric Company,General Electric Company,General Electric Company,General Electric Company,General Electric Company | General Electric Company CF6-80C2A1,General Electric Company CF6-80C2A2,General Electric Company CF6-80C2A3,General Electric Company CF6-80C2A5,General Electric Company CF6-80C2A5F,General Electric Company CF6-80C2A8,General Electric Company CF6-80C2B1,General Electric Company CF6-80C2B1F,General Electric Company CF6-80C2B1F1,General Electric Company CF6-80C2B1F2,General Electric Company CF6-80C2B2,General Electric Company CF6-80C2B2F,General Electric Company CF6-80C2B3F,General Electric Company CF6-80C2B4,General Electric Company CF6-80C2B4F,General Electric Company CF6-80C2B5F,General Electric Company CF6-80C2B6,General Electric Company CF6-80C2B6F,General Electric Company CF6-80C2B6FA,General Electric Company CF6-80C2B7F,General Electric Company CF6-80C2B8F,General Electric Company CF6-80C2D1F,General Electric Company CF6-80C2K1F,General Electric Company CF6-80C2L1F | CF6-80C2A1,CF6-80C2A2,CF6-80C2A3,CF6-80C2A5,CF6-80C2A5F,CF6-80C2A8,CF6-80C2B1,CF6-80C2B1F,CF6-80C2B1F1,CF6-80C2B1F2,CF6-80C2B2,CF6-80C2B2F,CF6-80C2B3F,CF6-80C2B4,CF6-80C2B4F,CF6-80C2B5F,CF6-80C2B6,CF6-80C2B6F,CF6-80C2B6FA,CF6-80C2B7F,CF6-80C2B8F,CF6-80C2D1F,CF6-80C2K1F,CF6-80C2L1F | Part 39 | Airworthiness Directives | 10/02/2009 | 1 | 2009-21-07.pdf | 47721 |
| 2009-21-06 | FAA-2009-0616 | 39-16043 | 11/20/2009 | 10/16/2009 | | | | 328 Support Services GmbH Dornier Model 328-100 and
-300 Airplanes | Equipment/furnishings.
| 328 Support Services GmbH | 328 Support Services GmbH,328 Support Services GmbH | 328 Support Services GmbH 328-100,328 Support Services GmbH 328-300 | 328-100,328-300 | Part 39 | Airworthiness Directives | 09/30/2009 | 1 | 2009-21-06.pdf | 33309 |
| 2009-21-05 | FAA-2009-0907 | 39-16042 | 11/02/2009 | 10/16/2009 | | | | Airbus Model A340-200 and -300 Series Airplanes | Engine exhaust. | Airbus | Airbus,Airbus,Airbus,Airbus,Airbus,Airbus | Airbus A340-211,Airbus A340-212,Airbus A340-213,Airbus A340-311,Airbus A340-312,Airbus A340-313 | A340-211,A340-212,A340-213,A340-311,A340-312,A340-313 | Part 39 | Airworthiness Directives | 09/30/2009 | 1 | 2009-21-05.pdf | 39287 |
| 2009-21-04 | FAA-2009-0045 | 39-16041 | 12/03/2009 | 10/29/2009 | | | | Rolls-Royce Deutschland Ltd & Co KG Model
BR700-715A1-30, BR700-715B1-30, and BR700-715C1-30 Turbofan Engines | Engine Failure
| Rolls-Royce Deutschland Ltd & Co KG | Rolls-Royce Deutschland Ltd & Co KG,Rolls-Royce Deutschland Ltd & Co KG,Rolls-Royce Deutschland Ltd & Co KG | Rolls-Royce Deutschland Ltd & Co KG BR700-715A1-30,Rolls-Royce Deutschland Ltd & Co KG BR700-715B1-30,Rolls-Royce Deutschland Ltd & Co KG BR700-715C1-30 | BR700-715A1-30,BR700-715B1-30,BR700-715C1-30 | Part 39 | Airworthiness Directives | 10/01/2009 | 1 | 2009-21-04.pdf | 34445 |
| 2009-21-03 | FAA-2009-0247 | 39-16040 | 11/20/2009 | 10/16/2009 | | | | Hamilton Sundstrand Power Systems T- 62T-46C12
Auxiliary Power Units | APU full- authority digital controller (FADEC) | Hamilton Sundstrand Power Systems | Bombardier Inc. | Hamilton Sundstrand Power Systems T-62T-46C12 | DHC-8-400 Series | Part 39 | Airworthiness Directives | 09/30/2009 | 1 | 2009-21-03.pdf | 28290 |
| 2009-21-02 | FAA-2009-0324 | 39-16039 | 12/01/2009 | 10/27/2009 | 2004-05-05 | | | Airbus Model A300 B4-601, B4-603, B4- 605R, B4-620,
B4-622, B4-622R, F4-605R, F4-622R, and C4-605R Variant F Series Airplanes
Equipped With Simmonds Precision Products, Inc., Fuel Quantity Indicating
System Sensors and In-Tank Harnesses Installed in Accordance With Supplemental
Type Certificate (STC) ST00092BO | Fuel
| Airbus | Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus | Airbus A300^ Model B4-601,Airbus A300^ Model B4-603,Airbus A300^ Model B4-605R,Airbus A300^ Model B4-620,Airbus A300^ Model B4-622,Airbus A300^ Model B4-622R,Airbus A300^ Model C4-605R Variant F,Airbus A300^ Model F4-605R,Airbus A300^ Model F4-622R | All Models, All Models, All Models, All Models, All Models, All Models, All Models,A300, Model B4-622,A300, Model C4-605R Variant F | Part 39 | Airworthiness Directives | 09/18/2009 | 1 | 2009-21-02.pdf | 35237 |
| 2009-21-01 | FAA-2009-0429 | 39-16038 | 11/17/2009 | 10/13/2009 | | | | Boeing Model 737-300 and 737-400 Series Airplanes | Fuselage | Boeing Company^ The | Boeing Company, The,Boeing Company, The | Boeing Company^ The 737-300 Series,Boeing Company^ The 737-400 Series | 737-300 Series,737-400 Series | Part 39 | Airworthiness Directives | 09/25/2009 | 1 | 2009-21-01.pdf | 38330 |
| 2009-20-14 | FAA-2009-0057 | 39-16037 | 11/17/2009 | 10/13/2009 | | | | Rolls-Royce plc (RR) RB211-535E4 Series Turbofan
Engines | Eddy current inspection (ECI) | Rolls-Royce plc | Rolls-Royce plc,Rolls-Royce plc,Rolls-Royce plc | Rolls-Royce plc RB211-535E4-37,Rolls-Royce plc RB211-535E4-B-37,Rolls-Royce plc RB211-535E4-B-75 | RB211-535E4-37,RB211-535E4-B-37,RB211-535E4-B-75 | Part 39 | Airworthiness Directives | 09/22/2009 | 1 | 2009-20-14.pdf | 30744 |
| 2009-20-13 | FAA-2009-0897 | 39-16036 | 10/21/2009 | 10/01/2009 | | | | Glaser-Dirks Flugzeugbau GmbH Model DG- 100 Gliders | Flight controls | Glaser-Dirks Flugzeugbau GmbH | Glaser-Dirks Flugzeugbau GmbH | Glaser-Dirks Flugzeugbau GmbH DG-100 | DG-100 | Part 39 | Airworthiness Directives | 09/24/2009 | 1 | 2009-20-13.pdf | 34139 |
| 2009-20-12 | FAA-2009-0293 | 39-16035 | 11/05/2009 | 10/01/2009 | | | | Boeing Model 747-100, -100B, -100B SUD, -200B, -200C,
-200F, -300, -400, -400D, -400F, and 747SR Series Airplanes | Flight controls | Boeing Company^ The | Boeing Company, The,Boeing Company, The,Boeing Company, The,Boeing Company, The,Boeing Company, The,Boeing Company, The,Boeing Company, The,Boeing Company, The,Boeing Company, The,Boeing Company, The,Boeing Company, The | Boeing Company^ The 747-100 Series,Boeing Company^ The 747-100B Series,Boeing Company^ The 747-100B SUD Series,Boeing Company^ The 747-200B Series,Boeing Company^ The 747-200C Series,Boeing Company^ The 747-200F Series,Boeing Company^ The 747-300 Series,Boeing Company^ The 747-400 Series,Boeing Company^ The 747-400D Series,Boeing Company^ The 747-400F Series,Boeing Company^ The 747SR Series | 747-100 Series,747-100B Series,747-100B SUD Series,747-200B Series,747-200C Series,747-200F Series,747-300 Series,747-400 Series,747-400D Series,747-400F Series,747SR Series | Part 39 | Airworthiness Directives | 09/18/2009 | 1 | 2009-20-12.pdf | 32793 |
| 2009-20-11 | FAA-2009-0521 | 39-16034 | 11/05/2009 | 10/01/2009 | | | | Boeing Model 737-300, -400, and -500 Series Airplanes
Equipped With a Digital Transient Suppression Device (DTSD) Installed in
Accordance With Supplemental Type Certificate (STC) ST00127BO | Fuel | Boeing Company^ The | Boeing Company, The,Boeing Company, The,Boeing Company, The | Boeing Company^ The 737-300 Series,Boeing Company^ The 737-400 Series,Boeing Company^ The 737-500 Series | 737-300 Series,737-400 Series,737-500 Series | Part 39 | Airworthiness Directives | 09/18/2009 | 1 | 2009-20-11.pdf | 37126 |
| 2009-20-10 | FAA-2009-0611 | 39-16033 | 11/17/2009 | 10/13/2009 | | | | Construcciones Aeronauticas, S.A. (CASA), Model
C-212-CB, C-212-CC, C-212-CD, and C-212-CE Airplanes | Auto Flight | Construcciones Aeronauticas^ S.A. | Construcciones Aeronauticas, S.A.,Construcciones Aeronauticas, S.A.,Construcciones Aeronauticas, S.A.,Construcciones Aeronauticas, S.A. | Construcciones Aeronauticas^ S.A. C-212-CB,Construcciones Aeronauticas^ S.A. C-212-CC,Construcciones Aeronauticas^ S.A. C-212-CD,Construcciones Aeronauticas^ S.A. C-212-CE | C-212-CB,C-212-CC,C-212-CD,C-212-CE | Part 39 | Airworthiness Directives | 09/18/2009 | 1 | 2009-20-10.pdf | 33403 |
| 2009-20-09 | FAA-2008-1363 | 39-16032 | 11/05/2009 | 10/01/2009 | | | | Boeing Model 767-200, -300, and -300F Series
Airplanes | Upper link fuse pins | Boeing Company^ The | Boeing Company, The,Boeing Company, The,Boeing Company, The | Boeing Company^ The 767-200 Series,Boeing Company^ The 767-300 Series,Boeing Company^ The 767-300F Series | 767-200 Series,767-300 Series,767-300F Series | Part 39 | Airworthiness Directives | 09/18/2009 | 1 | 2009-20-09.pdf | 38009 |
| 2009-20-08 | FAA-2008-0646 | 39-16031 | 11/05/2009 | 10/01/2009 | | | | Boeing Model 727 Airplanes | Fuel system | Boeing Company^ The | Boeing Company, The,Boeing Company, The,Boeing Company, The,Boeing Company, The,Boeing Company, The,Boeing Company, The | Boeing Company^ The 727-100 Series,Boeing Company^ The 727-100C Series,Boeing Company^ The 727-200 Series,Boeing Company^ The 727-200F Series,Boeing Company^ The 727 Series,Boeing Company^ The 727C Series | 727-100 Series,727-100C Series,727-200 Series,727-200F Series,727 Series,727C Series | Part 39 | Airworthiness Directives | 09/18/2009 | 1 | 2009-20-08.pdf | 34863 |
| 2009-20-07 | FAA-2009-0574 | 39-16030 | 11/03/2009 | 09/29/2009 | | | | DORNIER LUFTAHRT GmbH Models Dornier 228-100, Dornier
228-101, Dornier 228-200, Dornier 228-201, and Dornier 228-202 Airplanes | Landing gear
| Dornier Luftfahrt GmbH | Dornier Luftfahrt GmbH,Dornier Luftfahrt GmbH,Dornier Luftfahrt GmbH,Dornier Luftfahrt GmbH,Dornier Luftfahrt GmbH | Dornier Luftfahrt GmbH Dornier 228-100,Dornier Luftfahrt GmbH Dornier 228-101,Dornier Luftfahrt GmbH Dornier 228-200,Dornier Luftfahrt GmbH Dornier 228-201,Dornier Luftfahrt GmbH Dornier 228-202 | Dornier 228-100,Dornier 228-101,Dornier 228-200,Dornier 228-201,Dornier 228-202 | Part 39 | Airworthiness Directives | 09/21/2009 | 1 | 2009-20-07.pdf | 33841 |
| 2009-20-06 | FAA-2009-0431 | 39-16029 | 11/03/2009 | 09/29/2009 | 88-06-03 | | | Airbus Model A310-203 and -222 Airplanes and Model
A300 B4-620 Airplanes | Fuselage | Airbus | Airbus,Airbus,Airbus | Airbus A300B4-620,Airbus A310-203,Airbus A310-222 | A300B4-620,A310-203,A310-222 | Part 39 | Airworthiness Directives | 09/16/2009 | 1 | 2009-20-06.pdf | 41561 |
| 2009-20-05 | FAA-2007-0390 | 39-16028 | 11/03/2009 | 09/29/2009 | | | | Airbus Model A318, A319, A320, and A321 Series
Airplanes | Fuselage
| Airbus | Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus | Airbus A318 Model -111,Airbus A318 Model -112,Airbus A318 Model -121,Airbus A318 Model -122,Airbus A319 Model -111,Airbus A319 Model -112,Airbus A319 Model -113,Airbus A319 Model -114,Airbus A319 Model -115,Airbus A319 Model -131,Airbus A319 Model -132,Airbus A319 Model -133,Airbus A320 Model -111,Airbus A320 Model -211,Airbus A320 Model -212,Airbus A320 Model -214,Airbus A320 Model -231,Airbus A320 Model -232,Airbus A320 Model -233,Airbus A321 Model-212,Airbus A321 Model-213,Airbus A321 Model-232,Airbus A321 Model -111,Airbus A321 Model -112,Airbus A321 Model -131,Airbus A321 Model -211,Airbus A321 Model -231 | A318 Model -111,A318 Model -112,A318 Model -121,A318 Model -122,A319 Model -111,A319 Model -112,A319 Model -113,A319 Model -114,A319 Model -115,A319 Model -131,A319 Model -132,A319 Model -133,A320 Model -111,A320 Model -211,A320 Model -212,A320 Model -214,A320 Model -231,A320 Model -232,A320 Model -233,A321 Model-212,A321 Model-213,A321 Model-232,A321 Model -111,A321 Model -112,A321 Model -131,A321 Model -211,A321 Model -231 | Part 39 | Airworthiness Directives | 09/15/2009 | 1 | 2009-20-05.pdf | 37749 |
| 2009-20-04 | FAA-2009-0881 | 39-16027 | 10/19/2009 | 09/29/2009 | | | | Glaser-Dirks Flugzeugbau GmbH Model DG- 100 Gliders | Flight controls | Glaser-Dirks Flugzeugbau GmbH | Glaser-Dirks Flugzeugbau GmbH | Glaser-Dirks Flugzeugbau GmbH DG-100 | DG-100 | Part 39 | Airworthiness Directives | 09/17/2009 | 1 | 2009-20-04.pdf | 34648 |
| 2009-20-03 | FAA-2008-1117 | 39-16026 | 11/03/2009 | 09/29/2009 | | | | Boeing Model 727 Airplanes | Kickboard beam | Boeing Company^ The | Boeing Company, The,Boeing Company, The,Boeing Company, The,Boeing Company, The,Boeing Company, The,Boeing Company, The | Boeing Company^ The 727-100 Series,Boeing Company^ The 727-100C Series,Boeing Company^ The 727-200 Series,Boeing Company^ The 727-200F Series,Boeing Company^ The 727 Series,Boeing Company^ The 727C Series | 727-100 Series,727-100C Series,727-200 Series,727-200F Series,727 Series,727C Series | Part 39 | Airworthiness Directives | 09/15/2009 | 1 | 2009-20-03.pdf | 38643 |
| 2009-20-02 | FAA-2008-0682 | 39-16025 | 11/03/2009 | 09/29/2009 | | | | Boeing Model 767-200 and -300 Series Airplanes | Escape system latches
| Boeing Company^ The | Boeing Company, The,Boeing Company, The | Boeing Company^ The 767-200 Series,Boeing Company^ The 767-300 Series | 767-200 Series,767-300 Series | Part 39 | Airworthiness Directives | 09/11/2009 | 1 | 2009-20-02.pdf | 40586 |
| 2009-20-01 | FAA-2008-1325 | 39-16024 | 10/26/2009 | 09/21/2009 | | | | Boeing Model 727-281 Airplanes Equipped With
Auxiliary Fuel Tanks Installed in Accordance With Supplemental Type Certificate
SA3449NM | Auxiliary fuel tanks | Boeing Company^ The | Boeing Company, The,Boeing Company, The | Boeing Company^ The 727-200 Series,Boeing Company^ The 727-200F Series | 727-200 Series,727-200F Series | Part 39 | Airworthiness Directives | 09/11/2009 | 1 | 2009-20-01.pdf | 30908 |
| 2009-19-51 | Unknown | | | | | | | Emergency AD: Agusta S.p.A. (Agusta) Model AB139 and AW139 | Tailboom | Agusta S.p.A. | Agusta S.p.A.,Agusta S.p.A. | Agusta S.p.A. AB139,Agusta S.p.A. AW139 | AB139,AW139 | Part 39 | Emergency AD | 09/16/2009 | 1 | 2009-19-51.pdf | 25959 |
| 2009-19-07 | FAA-2009-0367 | 39-16023 | 10/07/2009 | 10/07/2009 | | | | Teledyne Continental Motors O-470, IO- 470, TSIO-470,
IO-520, TSIO-520, IO-550, and IOF-550 Series Reciprocating Engines | EQ3 cylinders | Teledyne Continental Motors | Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors | Teledyne Continental Motors IO-470-A,Teledyne Continental Motors IO-470-C,Teledyne Continental Motors IO-470-D,Teledyne Continental Motors IO-470-E,Teledyne Continental Motors IO-470-F,Teledyne Continental Motors IO-470-G,Teledyne Continental Motors IO-470-H,Teledyne Continental Motors IO-470-J,Teledyne Continental Motors IO-470-K,Teledyne Continental Motors IO-470-L,Teledyne Continental Motors IO-470-LO,Teledyne Continental Motors IO-470-M,Teledyne Continental Motors IO-470-N,Teledyne Continental Motors IO-470-P,Teledyne Continental Motors IO-470-R,Teledyne Continental Motors IO-470-S,Teledyne Continental Motors IO-470-T,Teledyne Continental Motors IO-470-U,Teledyne Continental Motors IO-470-V,Teledyne Continental Motors IO-470-VO,Teledyne Continental Motors IO-520-A,Teledyne Continental Motors IO-520-B,Teledyne Continental Motors IO-520-BA,Teledyne Continental Motors IO-520-BB,Teledyne Continental Motors IO-520-C,Teledyne Continental Motors IO-520-CB,Teledyne Continental Motors IO-520-D,Teledyne Continental Motors IO-520-E,Teledyne Continental Motors IO-520-F,Teledyne Continental Motors IO-520-J,Teledyne Continental Motors IO-520-K,Teledyne Continental Motors IO-520-L,Teledyne Continental Motors IO-520-M,Teledyne Continental Motors IO-520-MB,Teledyne Continental Motors IO-520-N,Teledyne Continental Motors IO-520-NB,Teledyne Continental Motors IO-550-A,Teledyne Continental Motors IO-550-B,Teledyne Continental Motors IO-550-C,Teledyne Continental Motors IO-550-D,Teledyne Continental Motors IO-550-E,Teledyne Continental Motors IO-550-F,Teledyne Continental Motors IO-550-G,Teledyne Continental Motors IO-550-L,Teledyne Continental Motors IO-550-N,Teledyne Continental Motors IO-550-P,Teledyne Continental Motors IO-550-R,Teledyne Continental Motors IOF-550-B,Teledyne Continental Motors IOF-550-C,Teledyne Continental Motors IOF-550-D,Teledyne Continental Motors IOF-550-E,Teledyne Continental Motors IOF-550-F,Teledyne Continental Motors IOF-550-L,Teledyne Continental Motors IOF-550-N,Teledyne Continental Motors IOF-550-P,Teledyne Continental Motors IOF-550-R,Teledyne Continental Motors O-470-11,Teledyne Continental Motors O-470-11-CI,Teledyne Continental Motors O-470-11B,Teledyne Continental Motors O-470-11B-CI,Teledyne Continental Motors O-470-13,Teledyne Continental Motors O-470-13A,Teledyne Continental Motors O-470-15,Teledyne Continental Motors O-470-2,Teledyne Continental Motors O-470-4,Teledyne Continental Motors O-470-A,Teledyne Continental Motors O-470-B,Teledyne Continental Motors O-470-B-CI,Teledyne Continental Motors O-470-E,Teledyne Continental Motors O-470-G,Teledyne Continental Motors O-470-G-CI,Teledyne Continental Motors O-470-H,Teledyne Continental Motors O-470-J,Teledyne Continental Motors O-470-K,Teledyne Continental Motors O-470-K-CI,Teledyne Continental Motors O-470-L,Teledyne Continental Motors O-470-L-CI,Teledyne Continental Motors O-470-M,Teledyne Continental Motors O-470-M-CI,Teledyne Continental Motors O-470-N,Teledyne Continental Motors O-470-P,Teledyne Continental Motors O-470-R,Teledyne Continental Motors O-470-S,Teledyne Continental Motors O-470-T,Teledyne Continental Motors O-470-U,Teledyne Continental Motors TSIO-470-B,Teledyne Continental Motors TSIO-470-C,Teledyne Continental Motors TSIO-470-D,Teledyne Continental Motors TSIO-520-A,Teledyne Continental Motors TSIO-520-AE,Teledyne Continental Motors TSIO-520-AF,Teledyne Continental Motors TSIO-520-B,Teledyne Continental Motors TSIO-520-BB,Teledyne Continental Motors TSIO-520-BE,Teledyne Continental Motors TSIO-520-C,Teledyne Continental Motors TSIO-520-CE,Teledyne Continental Motors TSIO-520-D,Teledyne Continental Motors TSIO-520-DB,Teledyne Continental Motors TSIO-520-E,Teledyne Continental Motors TSIO-520-EB,Teledyne Continental Motors TSIO-520-G,Teledyne Continental Motors TSIO-520-H,Teledyne Continental Motors TSIO-520-J,Teledyne Continental Motors TSIO-520-JB,Teledyne Continental Motors TSIO-520-K,Teledyne Continental Motors TSIO-520-KB,Teledyne Continental Motors TSIO-520-L,Teledyne Continental Motors TSIO-520-LB,Teledyne Continental Motors TSIO-520-M,Teledyne Continental Motors TSIO-520-N,Teledyne Continental Motors TSIO-520-NB,Teledyne Continental Motors TSIO-520-P,Teledyne Continental Motors TSIO-520-R,Teledyne Continental Motors TSIO-520-T,Teledyne Continental Motors TSIO-520-U,Teledyne Continental Motors TSIO-520-UB,Teledyne Continental Motors TSIO-520-VB,Teledyne Continental Motors TSIO-520-WB | IO-470-A,IO-470-C,IO-470-D,IO-470-E,IO-470-F,IO-470-G,IO-470-H,IO-470-J,IO-470-K,IO-470-L,IO-470-LO,IO-470-M,IO-470-N,IO-470-P,IO-470-R,IO-470-S,IO-470-T,IO-470-U,IO-470-V,IO-470-VO,IO-520-A,IO-520-B,IO-520-BA,IO-520-BB,IO-520-C,IO-520-CB,IO-520-D,IO-520-E,IO-520-F,IO-520-J,IO-520-K,IO-520-L,IO-520-M,IO-520-MB,IO-520-N,IO-520-NB,IO-550-A,IO-550-B,IO-550-C,IO-550-D,IO-550-E,IO-550-F,IO-550-G,IO-550-L,IO-550-N,IO-550-P,IO-550-R,IOF-550-B,IOF-550-C,IOF-550-D,IOF-550-E,IOF-550-F,IOF-550-L,IOF-550-N,IOF-550-P,IOF-550-R,O-470-11,O-470-11-CI,O-470-11B,O-470-11B-CI,O-470-13,O-470-13A,O-470-15,O-470-2,O-470-4,O-470-A,O-470-B,O-470-B-CI,O-470-E,O-470-G,O-470-G-CI,O-470-H,O-470-J,O-470-K,O-470-K-CI,O-470-L,O-470-L-CI,O-470-M,O-470-M-CI,O-470-N,O-470-P,O-470-R,O-470-S,O-470-T,O-470-U,TSIO-470-B,TSIO-470-C,TSIO-470-D,TSIO-520-A,TSIO-520-AE,TSIO-520-AF,TSIO-520-B,TSIO-520-BB,TSIO-520-BE,TSIO-520-C,TSIO-520-CE,TSIO-520-D,TSIO-520-DB,TSIO-520-E,TSIO-520-EB,TSIO-520-G,TSIO-520-H,TSIO-520-J,TSIO-520-JB,TSIO-520-K,TSIO-520-KB,TSIO-520-L,TSIO-520-LB,TSIO-520-M,TSIO-520-N,TSIO-520-NB,TSIO-520-P,TSIO-520-R,TSIO-520-T,TSIO-520-U,TSIO-520-UB,TSIO-520-VB,TSIO-520-WB | Part 39 | Airworthiness Directives | 09/08/2009 | 1 | 2009-19-07_Correction.pdf | 38030 |
| 2009-19-05 | FAA-2009-0136 | 39-16022 | 10/27/2009 | 09/22/2009 | | | | Boeing Model 747 Airplanes | Fuselage | Boeing Company^ The | Boeing Company, The,Boeing Company, The,Boeing Company, The,Boeing Company, The,Boeing Company, The,Boeing Company, The,Boeing Company, The,Boeing Company, The,Boeing Company, The,Boeing Company, The,Boeing Company, The,Boeing Company, The | Boeing Company^ The 747-100 Series,Boeing Company^ The 747-100B Series,Boeing Company^ The 747-100B SUD Series,Boeing Company^ The 747-200B Series,Boeing Company^ The 747-200C Series,Boeing Company^ The 747-200F Series,Boeing Company^ The 747-300 Series,Boeing Company^ The 747-400 Series,Boeing Company^ The 747-400D Series,Boeing Company^ The 747-400F Series,Boeing Company^ The 747SP Series,Boeing Company^ The 747SR Series | 747-100 Series,747-100B Series,747-100B SUD Series,747-200B Series,747-200C Series,747-200F Series,747-300 Series,747-400 Series,747-400D Series,747-400F Series,747SP Series,747SR Series | Part 39 | Airworthiness Directives | 09/01/2009 | 1 | 2009-19-05.pdf | 35354 |
| 2009-19-04 | FAA-2006-25173 | 39-16021 | 10/27/2009 | 09/22/2009 | 2008-08-01 | | | McCauley Propeller Systems Propeller Models
B5JFR36C1101/114GCA-0, C5JFR36C1102/L114GCA-0, B5JFR36C1103/ 114HCA-0, and
C5JFR36C1104/L114HCA-0 | Propeller blade | McCauley Propeller Systems | McCauley Propeller Systems,McCauley Propeller Systems,McCauley Propeller Systems,McCauley Propeller Systems | McCauley Propeller Systems B5JFR36C1101,McCauley Propeller Systems B5JFR36C1103,McCauley Propeller Systems C5JFR36C1102,McCauley Propeller Systems C5JFR36C1104 | B5JFR36C1101,B5JFR36C1103,C5JFR36C1102,C5JFR36C1104 | Part 39 | Airworthiness Directives | 09/03/2009 | 1 | 2009-19-04.pdf | 41866 |
| 2009-19-03 | FAA-2009-0817 | 39-16020 | 10/05/2009 | 09/14/2009 | 2009-13-10 | | | British Aerospace Regional Aircraft Model HP.137
Jetstream Mk.1, Jetstream Series 200 and 3101, and Jetstream Model 3201
Airplanes | Landing gear | British Aerospace Regional Aircraft | British Aerospace Regional Aircraft,British Aerospace Regional Aircraft,British Aerospace Regional Aircraft,British Aerospace Regional Aircraft | British Aerospace Regional Aircraft H.P. 137 Jetstream Mk. 1,British Aerospace Regional Aircraft Jetstream 3201,British Aerospace Regional Aircraft Jetstream Series 200,British Aerospace Regional Aircraft Jetstream Series 3101 | H.P. 137 Jetstream Mk. 1,Jetstream 3201,Jetstream Series 200,Jetstream Series 3101 | Part 39 | Airworthiness Directives | 09/01/2009 | 1 | 2009-19-03.pdf | 38052 |
| 2009-19-02 | FAA-2009-0212 | 39-16019 | 10/14/2009 | 09/09/2009 | | | | Boeing Model 737-600, -700, -700C, - 800, -900 and
-900ER Series Airplanes | Flight controls
| Boeing Company^ The | Boeing Company, The,Boeing Company, The,Boeing Company, The,Boeing Company, The,Boeing Company, The,Boeing Company, The | Boeing Company^ The 737-600 Series,Boeing Company^ The 737-700 Series,Boeing Company^ The 737-700C Series,Boeing Company^ The 737-800 Series,Boeing Company^ The 737-900 Series,Boeing Company^ The 737-900ER Series | 737-600 Series,737-700 Series,737-700C Series,737-800 Series,737-900 Series,737-900ER Series | Part 39 | Airworthiness Directives | 08/31/2009 | 1 | 2009-19-02.pdf | 34308 |
| 2009-19-01 | FAA-2009-0397 | 39-16018 | 10/14/2009 | 09/09/2009 | | | | Airbus Model A300 B2-1C, B2-203, B2K- 3C, B4-103,
B4-203, and B4-2C Airplanes | Wings
| Airbus | Airbus,Airbus,Airbus,Airbus,Airbus,Airbus | Airbus A300 Model B2-1C,Airbus A300 Model B2-203,Airbus A300 Model B2K-3C,Airbus A300 Model B4-103,Airbus A300 Model B4-203,Airbus A300 Model B4-2C | A300 Model B2-1C,A300 Model B2-203,A300 Model B2K-3C,A300 Model B4-103,A300 Model B4-203,A300 Model B4-2C | Part 39 | Airworthiness Directives | 08/31/2009 | 1 | 2009-19-01.pdf | 35482 |
| 2009-18-20 | FAA-2009-0264 | 39-16017 | 10/14/2009 | 09/09/2009 | | | | Airbus Model A330-300, A340-200, and A340-300 Series
Airplanes | Flight controls | Airbus | Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus | Airbus A330-301,Airbus A330-302,Airbus A330-303,Airbus A330-321,Airbus A330-322,Airbus A330-323,Airbus A330-341,Airbus A330-342,Airbus A340-211,Airbus A340-212,Airbus A340-213,Airbus A340-311,Airbus A340-312,Airbus A340-313 | A330-301,A330-302,A330-303,A330-321,A330-322,A330-323,A330-341,A330-342,A340-211,A340-212,A340-213,A340-311,A340-312,A340-313 | Part 39 | Airworthiness Directives | 08/26/2009 | 1 | 2009-18-20.pdf | 41556 |
| 2009-18-19 | FAA-2009-0381 | 39-16016 | 10/14/2009 | 09/09/2009 | | | | Airbus Model A330-200 and -300 Series Airplanes and
Model A340-200 and -300 Series Airplanes | Fuel | Airbus | Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus | Airbus A330-201,Airbus A330-202,Airbus A330-203,Airbus A330-223,Airbus A330-243,Airbus A330-301,Airbus A330-302,Airbus A330-303,Airbus A330-321,Airbus A330-322,Airbus A330-323,Airbus A330-341,Airbus A330-342,Airbus A330-343,Airbus A340-211,Airbus A340-212,Airbus A340-213,Airbus A340-311,Airbus A340-312,Airbus A340-313 | A330-201,A330-202,A330-203,A330-223,A330-243,A330-301,A330-302,A330-303,A330-321,A330-322,A330-323,A330-341,A330-342,A330-343,A340-211,A340-212,A340-213,A340-311,A340-312,A340-313 | Part 39 | Airworthiness Directives | 08/26/2009 | 1 | 2009-18-19.pdf | 34359 |
| 2009-18-18 | FAA-2009-0786 | 39-16014 | 09/24/2009 | 09/09/2009 | | | | ATR Model ATR42 and ATR72 Airplanes | Windows | ATR – GIE Avions de Transport Régional | ATR – GIE Avions de Transport Régio,ATR – GIE Avions de Transport Régio,ATR – GIE Avions de Transport Régio,ATR – GIE Avions de Transport Régio,ATR – GIE Avions de Transport Régio,ATR – GIE Avions de Transport Régio,ATR – GIE Avions de Transport Régio,ATR – GIE Avions de Transport Régio,ATR – GIE Avions de Transport Régio,ATR – GIE Avions de Transport Régio,ATR – GIE Avions de Transport Régio | ATR – GIE Avions de Transport Régional ATR42-200,ATR – GIE Avions de Transport Régional ATR42-300,ATR – GIE Avions de Transport Régional ATR42-320,ATR – GIE Avions de Transport Régional ATR42-500,ATR – GIE Avions de Transport Régional ATR72-101,ATR – GIE Avions de Transport Régional ATR72-102,ATR – GIE Avions de Transport Régional ATR72-201,ATR – GIE Avions de Transport Régional ATR72-202,ATR – GIE Avions de Transport Régional ATR72-211,ATR – GIE Avions de Transport Régional ATR72-212,ATR – GIE Avions de Transport Régional ATR72-212A | ATR42-200,ATR42-300,ATR42-320,ATR42-500,ATR72-101,ATR72-102,ATR72-201,ATR72-202,ATR72-211,ATR72-212,ATR72-212A | Part 39 | Airworthiness Directives | 08/26/2009 | 1 | 2009-18-18.pdf | 38225 |
| 2009-18-17 | FAA-2009-0804 | 39-16013 | 09/21/2009 | 09/04/2009 | | | | Agusta S.p.A. Model AB412 and AB412 EP Helicopters | Miscellaneous Hardware
| Agusta S.p.A. | Agusta S.p.A.,Agusta S.p.A. | Agusta S.p.A. AB412,Agusta S.p.A. AB412 EP | AB412,AB412 EP | Part 39 | Airworthiness Directives | 08/26/2009 | 1 | 2009-18-17.pdf | 30745 |
| 2009-18-16 | FAA-2009-0465 | 39-16012 | 10/14/2009 | 09/09/2009 | 2006-02-06 | | | Airbus Model A310-203, -204, -221, - 222, -304, -322,
-324, and -325 Airplanes | Fuselage | Airbus | Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus | Airbus A310-203,Airbus A310-204,Airbus A310-221,Airbus A310-222,Airbus A310-304,Airbus A310-322,Airbus A310-324,Airbus A310-325 | A310-203,A310-204,A310-221,A310-222,A310-304,A310-322,A310-324,A310-325 | Part 39 | Airworthiness Directives | 08/24/2009 | 1 | 2009-18-16.pdf | 38454 |
| 2009-18-15 | FAA-2009-0292 | 39-16011 | 10/27/2009 | 09/22/2009 | 87-16-06 | | | Airbus Model A300, A310, and A300-600 Series
Airplanes | Landing gear | Airbus | Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus | Airbus A300 Model B2-1A,Airbus A300 Model B2-1C,Airbus A300 Model B2-203,Airbus A300 Model B2K-3C,Airbus A300 Model B4-103,Airbus A300 Model B4-203,Airbus A300 Model B4-2C,Airbus A300B4-601,Airbus A300B4-603,Airbus A300B4-605R,Airbus A300B4-620,Airbus A300B4-622R,Airbus A300F4-605R,Airbus A300F4-622R,Airbus A300^ Model B4-622,Airbus A300^ Model C4-605 Variant F,Airbus A310-203,Airbus A310-204,Airbus A310-221,Airbus A310-222,Airbus A310-304,Airbus A310-322,Airbus A310-324,Airbus A310-325 | A300 Model B2-1A,A300 Model B2-1C,A300 Model B2-203,A300 Model B2K-3C,A300 Model B4-103,A300 Model B4-203,A300 Model B4-2C,A300B4-601,A300B4-603,A300B4-605R,A300B4-620,A300B4-622R,A300F4-605R,A300F4-622R,A300, Model B4-622,A300, Model C4-605 Variant F,A310-203,A310-204,A310-221,A310-222,A310-304,A310-322,A310-324,A310-325 | Part 39 | Airworthiness Directives | 08/24/2009 | 1 | 2009-18-15.pdf | 63153 |
| 2009-18-14 | FAA-2009-0522 | 39-16010 | 10/14/2009 | 09/09/2009 | 2004-09-16 | | | 328 Support Services GmbH Dornier Model 328-100 and
-300 Airplanes | Flight controls
| 328 Support Services GmbH | 328 Support Services GmbH,328 Support Services GmbH | 328 Support Services GmbH 328-100,328 Support Services GmbH 328-300 | 328-100,328-300 | Part 39 | Airworthiness Directives | 08/24/2009 | 1 | 2009-18-14.pdf | 39273 |
| 2009-18-13 | FAA-2009-0771 | 39-16009 | 10/14/2009 | 09/09/2009 | | | | Rolls-Royce plc. (RR) RB211 Trent 900 Series Turbofan
Engines | HP Turbine Nozzle Guide Vane (NGV) Convex Surfaces
| Rolls-Royce plc | Rolls-Royce plc,Rolls-Royce plc,Rolls-Royce plc,Rolls-Royce plc,Rolls-Royce plc,Rolls-Royce plc,Rolls-Royce plc | Rolls-Royce plc RB211-TRENT 970-84,Rolls-Royce plc RB211-TRENT 970B-84,Rolls-Royce plc RB211-TRENT 972-84,Rolls-Royce plc RB211-TRENT 972B-84,Rolls-Royce plc RB211-TRENT 977-84,Rolls-Royce plc RB211-TRENT 977B-84,Rolls-Royce plc RB211-TRENT 980-84 | RB211-TRENT 970-84,RB211-TRENT 970B-84,RB211-TRENT 972-84,RB211-TRENT 972B-84,RB211-TRENT 977-84,RB211-TRENT 977B-84,RB211-TRENT 980-84 | Part 39 | Airworthiness Directives | 08/20/2009 | 1 | 2009-18-13.pdf | 32108 |
| 2009-18-12 | FAA-2009-0526 | 39-16008 | 10/14/2009 | 09/09/2009 | | | | Bombardier Model DHC-8-400 Series Airplanes | Propellers/Propulsors
| Bombardier Inc. | Bombardier Inc. | Bombardier Inc. DHC-8-400 Series | DHC-8-400 Series | Part 39 | Airworthiness Directives | 08/18/2009 | 1 | 2009-18-12.pdf | 33081 |
| 2009-18-11 | FAA-2009-0515 | 39-16007 | 10/14/2009 | 09/09/2009 | | | | Fokker Model F.28 Mark 0070 and 0100 Series Airplanes | Placards and Markings, and Doors
| Fokker Services | Fokker Services,Fokker Services | Fokker Services F.28 Mark 0070,Fokker Services F.28 Mark 0100 | F.28 Mark 0070,F.28 Mark 0100 | Part 39 | Airworthiness Directives | 08/18/2009 | 1 | 2009-18-11.pdf | 36502 |
| 2009-18-10 | FAA-2009-0476 | 39-16006 | 10/14/2009 | 09/09/2009 | 2008-17-10 | | | Boeing Model 707 Airplanes, and Model 720 and 720B
Series Airplanes | Wings
| Boeing Company^ The | Boeing Company, The,Boeing Company, The,Boeing Company, The,Boeing Company, The,Boeing Company, The,Boeing Company, The,Boeing Company, The,Boeing Company, The,Boeing Company, The,Boeing Company, The | Boeing Company^ The 707-100 Long Body,Boeing Company^ The 707-100B Long Body,Boeing Company^ The 707-100B Short Body,Boeing Company^ The 707-200,Boeing Company^ The 707-300 Series,Boeing Company^ The 707-300B Series,Boeing Company^ The 707-300C Series,Boeing Company^ The 707-400 Series,Boeing Company^ The 720 Series,Boeing Company^ The 720B Series | 707-100 Long Body,707-100B Long Body,707-100B Short Body,707-200,707-300 Series,707-300B Series,707-300C Series,707-400 Series,720 Series,720B Series | Part 39 | Airworthiness Directives | 08/18/2009 | 1 | 2009-18-10.pdf | 35357 |
| 2009-18-09 | FAA-2009-0563 | 39-16005 | 09/22/1999 | 09/09/2009 | 99-20-01 | | | Fokker Model F.28 Mark 0070 and 0100 Airplanes | Instruments and Engine Exhaust
| Fokker Services | Fokker Services,Fokker Services | Fokker Services F.28 Mark 0070,Fokker Services F.28 Mark 0100 | F.28 Mark 0070,F.28 Mark 0100 | Part 39 | Airworthiness Directives | 08/18/2009 | 1 | 2009-18-09.pdf | 39290 |
| 2009-18-08 | FAA-2009-0781 | 39-16004 | 09/08/2009 | 09/03/2009 | | | | Airbus Model A330-200 and -300 Series Airplanes,
Model A340-200 and -300 Series Airplanes, and Model A340-541 and -642 Airplanes | Navigation | Airbus | Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus | Airbus A330-201,Airbus A330-202,Airbus A330-203,Airbus A330-223,Airbus A330-243,Airbus A330-301,Airbus A330-302,Airbus A330-303,Airbus A330-321,Airbus A330-322,Airbus A330-323,Airbus A330-341,Airbus A330-342,Airbus A330-343,Airbus A340-211,Airbus A340-212,Airbus A340-213,Airbus A340-311,Airbus A340-312,Airbus A340-313,Airbus A340-541,Airbus A340-642 | A330-201,A330-202,A330-203,A330-223,A330-243,A330-301,A330-302,A330-303,A330-321,A330-322,A330-323,A330-341,A330-342,A330-343,A340-211,A340-212,A340-213,A340-311,A340-312,A340-313,A340-541,A340-642 | Part 39 | Airworthiness Directives | 08/24/2009 | 1 | 2009-18-08.pdf | 40199 |
| 2009-18-07 | FAA-2009-0477 | 39-16003 | 10/01/2009 | 08/27/2009 | 2005-20-30 | | | Boeing Model 747-100, -100B, -100B SUD, -200B, and
-300 Series Airplanes; and Model 747SP and 747SR Series Airplanes | Fuselage | Boeing Company^ The | Boeing Company, The,Boeing Company, The,Boeing Company, The,Boeing Company, The,Boeing Company, The,Boeing Company, The,Boeing Company, The | Boeing Company^ The 747-100 Series,Boeing Company^ The 747-100B Series,Boeing Company^ The 747-100B SUD Series,Boeing Company^ The 747-200B Series,Boeing Company^ The 747-300 Series,Boeing Company^ The 747SP Series,Boeing Company^ The 747SR Series | 747-100 Series,747-100B Series,747-100B SUD Series,747-200B Series,747-300 Series,747SP Series,747SR Series | Part 39 | Airworthiness Directives | 08/17/2009 | 1 | 2009-18-07.pdf | 37492 |
| 2009-18-06 | FAA-2009-0386 | 39-16002 | 10/01/2009 | 08/27/2009 | | | | Construcciones Aeronauticas, S.A. (CASA), Model
CN-235, CN-235-100, CN-235-200, and CN-235-300 Airplanes | Ice and rain protection
| Construcciones Aeronauticas^ S.A. | Construcciones Aeronauticas, S.A.,Construcciones Aeronauticas, S.A.,Construcciones Aeronauticas, S.A.,Construcciones Aeronauticas, S.A. | Construcciones Aeronauticas^ S.A. CN-235,Construcciones Aeronauticas^ S.A. CN-235-100,Construcciones Aeronauticas^ S.A. CN-235-200,Construcciones Aeronauticas^ S.A. CN-235-300 | CN-235,CN-235-100,CN-235-200,CN-235-300 | Part 39 | Airworthiness Directives | 08/17/2009 | 1 | 2009-18-06.pdf | 33234 |
| 2009-18-05 | FAA-2009-0496 | 39-16001 | 10/01/2009 | 08/27/2009 | | | | Fokker Model F.27 Mark 050 and F.28 Mark 0100
Airplanes | Electrical power
| Fokker Services | Fokker Services,Fokker Services | Fokker Services F27 Mark 050,Fokker Services F.28 Mark 0100 | F27 Mark 050,F.28 Mark 0100 | Part 39 | Airworthiness Directives | 08/17/2009 | 1 | 2009-18-05.pdf | 39089 |
| 2009-18-04 | FAA-2009-0489 | 39-16000 | 10/01/2009 | 08/27/2009 | | | | Air Tractor, Inc. Models AT-802 and AT- 802A
Airplanes | Rudder-aileron interconnect | Air Tractor^ Inc. | Air Tractor, Inc.,Air Tractor, Inc. | Air Tractor^ Inc. AT-802,Air Tractor^ Inc. AT-802A | AT-802,AT-802A | Part 39 | Airworthiness Directives | 08/18/2009 | 1 | 2009-18-04.pdf | 29085 |
| 2009-18-03 | FAA-2009-0622 | 39-15999 | 10/01/2009 | 08/27/2009 | 2007-19-14 | | | Pilatus Aircraft Ltd. Models PC-6, PC- 6-H1, PC-6-H2,
PC-6/350, PC-6/350-H1, PC-6/350-H2, PC-6/A, PC-6/A-H1, PC-6/A-H2, PC-6/B-H2,
PC-6/B1-H2, PC-6/B2-H2, PC-6/B2-H4, PC-6/C-H2, and PC-6/C1-H2 Airplanes | Wings | Pilatus Aircraft Limited | Pilatus Aircraft Limited,Pilatus Aircraft Limited,Pilatus Aircraft Limited,Pilatus Aircraft Limited,Pilatus Aircraft Limited,Pilatus Aircraft Limited,Pilatus Aircraft Limited,Pilatus Aircraft Limited,Pilatus Aircraft Limited,Pilatus Aircraft Limited,Pilatus Aircraft Limited,Pilatus Aircraft Limited,Pilatus Aircraft Limited,Pilatus Aircraft Limited,Pilatus Aircraft Limited | Pilatus Aircraft Limited PC-6,Pilatus Aircraft Limited PC-6-H1,Pilatus Aircraft Limited PC-6-H2,Pilatus Aircraft Limited PC-6/350,Pilatus Aircraft Limited PC-6/350-H1,Pilatus Aircraft Limited PC-6/350-H2,Pilatus Aircraft Limited PC-6/A,Pilatus Aircraft Limited PC-6/A-H1,Pilatus Aircraft Limited PC-6/A-H2,Pilatus Aircraft Limited PC-6/B-H2,Pilatus Aircraft Limited PC-6/B1-H2,Pilatus Aircraft Limited PC-6/B2-H2,Pilatus Aircraft Limited PC-6/B2-H4,Pilatus Aircraft Limited PC-6/C-H2,Pilatus Aircraft Limited PC-6/C1-H2 | PC-6,PC-6-H1,PC-6-H2,PC-6/350,PC-6/350-H1,PC-6/350-H2,PC-6/A,PC-6/A-H1,PC-6/A-H2,PC-6/B-H2,PC-6/B1-H2,PC-6/B2-H2,PC-6/B2-H4,PC-6/C-H2,PC-6/C1-H2 | Part 39 | Airworthiness Directives | 08/18/2009 | 1 | 2009-18-03.pdf | 38622 |
| 2009-18-02 | FAA-2007-28035 | 39-15998 | 10/01/2009 | 08/27/2009 | | | | Boeing Model 767 Airplanes | Auxiliary fuel tank, main fuel tanks, and surge tanks | Boeing Company^ The | Boeing Company, The,Boeing Company, The,Boeing Company, The,Boeing Company, The | Boeing Company^ The 767-200 Series,Boeing Company^ The 767-300 Series,Boeing Company^ The 767-300F Series,Boeing Company^ The 767-400ER Series | 767-200 Series,767-300 Series,767-300F Series,767-400ER Series | Part 39 | Airworthiness Directives | 08/07/2009 | 1 | 2009-18-02.pdf | 32659 |
| 2009-18-01 | FAA-2008-0174 | 39-15997 | 10/01/2009 | 08/27/2009 | | | | CFM International, S.A. CFM56-5B1/P; - 5B2/P; -5B3/P;
-5B3/P1; -5B4/P; -5B4/P1; -5B5/P; -5B6/P; -5B7/P; -5B8/ P; -5B9/P; -5B1/3;
-5B2/3; -5B3/3; -5B4/3; -5B5/3; -5B6/3; -5B7/3; - 5B8/3; -5B9/3; -5B3/3B1; and
-5B4/3B1 Turbofan Engines | LP turbine rear frames | CFM International^ S.A. | CFM International, S.A.,CFM International, S.A.,CFM International, S.A.,CFM International, S.A.,CFM International, S.A.,CFM International, S.A.,CFM International, S.A.,CFM International, S.A.,CFM International, S.A.,CFM International, S.A.,CFM International, S.A.,CFM International, S.A.,CFM International, S.A.,CFM International, S.A.,CFM International, S.A.,CFM International, S.A.,CFM International, S.A.,CFM International, S.A.,CFM International, S.A.,CFM International, S.A.,CFM International, S.A.,CFM International, S.A. | CFM International^ S.A. CFM56-5B1/3,CFM International^ S.A. CFM56-5B1/P,CFM International^ S.A. CFM56-5B2/3,CFM International^ S.A. CFM56-5B2/P,CFM International^ S.A. CFM56-5B3/3,CFM International^ S.A. CFM56-5B3/3B1,CFM International^ S.A. CFM56-5B3/P,CFM International^ S.A. CFM56-5B3/P1,CFM International^ S.A. CFM56-5B4/3,CFM International^ S.A. CFM56-5B4/3B1,CFM International^ S.A. CFM56-5B4/P,CFM International^ S.A. CFM56-5B4/P1,CFM International^ S.A. CFM56-5B5/3,CFM International^ S.A. CFM56-5B5/P,CFM International^ S.A. CFM56-5B6/3,CFM International^ S.A. CFM56-5B6/P,CFM International^ S.A. CFM56-5B7/3,CFM International^ S.A. CFM56-5B7/P,CFM International^ S.A. CFM56-5B8/3,CFM International^ S.A. CFM56-5B8/P,CFM International^ S.A. CFM56-5B9/3,CFM International^ S.A. CFM56-5B9/P | CFM56-5B1/3,CFM56-5B1/P,CFM56-5B2/3,CFM56-5B2/P,CFM56-5B3/3,CFM56-5B3/3B1,CFM56-5B3/P,CFM56-5B3/P1,CFM56-5B4/3,CFM56-5B4/3B1,CFM56-5B4/P,CFM56-5B4/P1,CFM56-5B5/3,CFM56-5B5/P,CFM56-5B6/3,CFM56-5B6/P,CFM56-5B7/3,CFM56-5B7/P,CFM56-5B8/3,CFM56-5B8/P,CFM56-5B9/3,CFM56-5B9/P | Part 39 | Airworthiness Directives | 08/17/2009 | 1 | 2009-18-01.pdf | 30928 |
| 2009-17-05 | FAA-2009-0555 | 39-15996 | 09/01/2009 | 08/17/2009 | | | | Honeywell International Inc. TPE331-10 and TPE331-11
Series Turboprop Engines | First stage turbine disks | Honeywell International Inc. | Honeywell International Inc.,Honeywell International Inc.,Honeywell International Inc.,Honeywell International Inc.,Honeywell International Inc.,Honeywell International Inc.,Honeywell International Inc.,Honeywell International Inc.,Honeywell International Inc.,Honeywell International Inc.,Honeywell International Inc.,Honeywell International Inc.,Honeywell International Inc.,Honeywell International Inc.,Honeywell International Inc.,Honeywell International Inc.,Honeywell International Inc.,Honeywell International Inc.,Honeywell International Inc.,Honeywell International Inc.,Honeywell International Inc.,Honeywell International Inc.,Honeywell International Inc. | Honeywell International Inc. TPE331-10,Honeywell International Inc. TPE331-10A,Honeywell International Inc. TPE331-10AV,Honeywell International Inc. TPE331-10B,Honeywell International Inc. TPE331-10G,Honeywell International Inc. TPE331-10GP,Honeywell International Inc. TPE331-10GR,Honeywell International Inc. TPE331-10GT,Honeywell International Inc. TPE331-10J,Honeywell International Inc. TPE331-10N,Honeywell International Inc. TPE331-10P,Honeywell International Inc. TPE331-10R,Honeywell International Inc. TPE331-10T,Honeywell International Inc. TPE331-10U,Honeywell International Inc. TPE331-10UA,Honeywell International Inc. TPE331-10UF,Honeywell International Inc. TPE331-10UG,Honeywell International Inc. TPE331-10UGR,Honeywell International Inc. TPE331-10UJ,Honeywell International Inc. TPE331-10UK,Honeywell International Inc. TPE331-10UR,Honeywell International Inc. TPE331-11U,Honeywell International Inc. TPE331-11UA | TPE331-10,TPE331-10A,TPE331-10AV,TPE331-10B,TPE331-10G,TPE331-10GP,TPE331-10GR,TPE331-10GT,TPE331-10J,TPE331-10N,TPE331-10P,TPE331-10R,TPE331-10T,TPE331-10U,TPE331-10UA,TPE331-10UF,TPE331-10UG,TPE331-10UGR,TPE331-10UJ,TPE331-10UK,TPE331-10UR,TPE331-11U,TPE331-11UA | Part 39 | Airworthiness Directives | 08/11/2009 | 1 | 2009-17-05.pdf | 30016 |
| 2009-17-04 | FAA-2009-0004 | 39-15995 | 09/22/2009 | 08/18/2009 | | | | Airbus Model A318, A319, A320, and A321 Series
Airplanes | Flight controls
| Airbus | Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus | Airbus A318 Model -111,Airbus A318 Model -112,Airbus A318 Model -121,Airbus A318 Model -122,Airbus A319 Model -111,Airbus A319 Model -112,Airbus A319 Model -113,Airbus A319 Model -114,Airbus A319 Model -115,Airbus A319 Model -131,Airbus A319 Model -132,Airbus A319 Model -133,Airbus A320 Model -111,Airbus A320 Model -211,Airbus A320 Model -212,Airbus A320 Model -214,Airbus A320 Model -231,Airbus A320 Model -232,Airbus A320 Model -233,Airbus A321 Model-212,Airbus A321 Model-213,Airbus A321 Model-232,Airbus A321 Model -111,Airbus A321 Model -112,Airbus A321 Model -131,Airbus A321 Model -211,Airbus A321 Model -231 | A318 Model -111,A318 Model -112,A318 Model -121,A318 Model -122,A319 Model -111,A319 Model -112,A319 Model -113,A319 Model -114,A319 Model -115,A319 Model -131,A319 Model -132,A319 Model -133,A320 Model -111,A320 Model -211,A320 Model -212,A320 Model -214,A320 Model -231,A320 Model -232,A320 Model -233,A321 Model-212,A321 Model-213,A321 Model-232,A321 Model -111,A321 Model -112,A321 Model -131,A321 Model -211,A321 Model -231 | Part 39 | Airworthiness Directives | 08/07/2009 | 1 | 2009-17-04.pdf | 36927 |
| 2009-17-03 | FAA-2009-0532 | 39-15994 | 09/22/2009 | 08/18/2009 | | | | BAE Systems (Operations) Limited Model BAe 146 and
Avro 146-RJ Airplanes | Fuselage | BAE Systems (Operations) Limited | BAE Systems (Operations) Limited,BAE Systems (Operations) Limited,BAE Systems (Operations) Limited,BAE Systems (Operations) Limited,BAE Systems (Operations) Limited,BAE Systems (Operations) Limited | BAE Systems (Operations) Limited Avro 146-RJ100A,BAE Systems (Operations) Limited Avro 146-RJ70A,BAE Systems (Operations) Limited Avro 146-RJ85A,BAE Systems (Operations) Limited BAe 146-100A,BAE Systems (Operations) Limited BAe 146-200A,BAE Systems (Operations) Limited BAe 146-300A | Avro 146-RJ100A,Avro 146-RJ70A,Avro 146-RJ85A,BAe 146-100A,BAe 146-200A,BAe 146-300A | Part 39 | Airworthiness Directives | 08/04/2009 | 1 | 2009-17-03.pdf | 34810 |
| 2009-17-02 | FAA-2009-0447 | 39-15993 | 09/22/2009 | 08/18/2009 | | | | Saab AB, Saab Aerosystems Model SAAB 340A
(SAAB/SF340A) and SAAB 340B Airplanes | Fuel | Saab AB^ Saab Aerosystems | Saab AB, Saab Aerosystems,Saab AB, Saab Aerosystems | Saab AB^ Saab Aerosystems 340A (SAAB SF340A),Saab AB^ Saab Aerosystems SAAB 340B | 340A (SAAB SF340A),SAAB 340B | Part 39 | Airworthiness Directives | 08/03/2009 | 1 | 2009-17-02.pdf | 33712 |
| 2009-17-01 | FAA-2009-0683 | 39-15991 | 08/26/2009 | 08/11/2009 | | | | Gulfstream Model G-IV, GIV-X, and GV-SP Series
Airplanes and Model GV Airplanes | Airborne Auxiliary Power | Gulfstream Aerospace Corporation | Gulfstream Aerospace Corporation,Gulfstream Aerospace Corporation,Gulfstream Aerospace Corporation,Gulfstream Aerospace Corporation | Gulfstream Aerospace Corporation G-IV,Gulfstream Aerospace Corporation GIV-X,Gulfstream Aerospace Corporation GV,Gulfstream Aerospace Corporation GV-SP | G-IV,GIV-X,GV,GV-SP | Part 39 | Airworthiness Directives | 07/31/2009 | 1 | 2009-17-01.pdf | 43971 |
| 2009-16-14 | FAA-2008-1213 | 39-15987 | 09/09/2009 | 08/05/2009 | 2005-20-03 | | | Boeing Model 737-100, -200, -200C, - 300, -400, and
-500 Series Airplanes | Forward entry door | Boeing Company^ The | Boeing Company, The,Boeing Company, The,Boeing Company, The,Boeing Company, The,Boeing Company, The,Boeing Company, The | Boeing Company^ The 737-100 Series,Boeing Company^ The 737-200 Series,Boeing Company^ The 737-200C Series,Boeing Company^ The 737-300 Series,Boeing Company^ The 737-400 Series,Boeing Company^ The 737-500 Series | 737-100 Series,737-200 Series,737-200C Series,737-300 Series,737-400 Series,737-500 Series | Part 39 | Airworthiness Directives | 07/23/2009 | 1 | 2009-16-14.pdf | 35232 |
| 2009-16-07 | FAA-2008-1143 | 39-15990 | 09/22/2009 | 08/18/2009 | 2006-10-17 | | | Boeing Model 737-600, -700, -700C, - 800, and -900
Series Airplanes | Standby compass bracket assembly | Boeing Company^ The | Boeing Company, The,Boeing Company, The,Boeing Company, The,Boeing Company, The,Boeing Company, The | Boeing Company^ The 737-600 Series,Boeing Company^ The 737-700 Series,Boeing Company^ The 737-700C Series,Boeing Company^ The 737-800 Series,Boeing Company^ The 737-900 Series | 737-600 Series,737-700 Series,737-700C Series,737-800 Series,737-900 Series | Part 39 | Airworthiness Directives | 08/07/2009 | 1 | 2009-16-07.pdf | 42193 |
| 2009-16-06 | FAA-2007-29173 | 39-15989 | 09/09/2009 | 08/05/2009 | | | | Boeing Model 767 Airplanes | Fuel tank systems | Boeing Company^ The | Boeing Company, The,Boeing Company, The,Boeing Company, The,Boeing Company, The | Boeing Company^ The 767-200 Series,Boeing Company^ The 767-300 Series,Boeing Company^ The 767-300F Series,Boeing Company^ The 767-400ER Series | 767-200 Series,767-300 Series,767-300F Series,767-400ER Series | Part 39 | Airworthiness Directives | 07/24/2009 | 1 | 2009-16-06.pdf | 47527 |
| 2009-16-05 | FAA-2009-0691 | 39-15988 | 08/20/2009 | 08/05/2009 | | | | Fokker Model F.27 Mark 050 Airplanes | Flight Controls.
| Fokker Services | Fokker Services | Fokker Services F27 Mark 050 | F27 Mark 050 | Part 39 | Airworthiness Directives | 07/24/2009 | 1 | 2009-16-05.pdf | 36079 |
| 2009-16-03 | FAA-2007-0051 | 39-15986 | 09/09/2009 | 08/05/2009 | | | | Teledyne Continental Motors (TCM) IO- 520, TSIO-520,
and IO-550 Series Reciprocating Engines With Superior Air Parts, Inc. (SAP)
Cylinder Assemblies Installed | Cylinder assemblies
| Teledyne Continental Motors | Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors,Teledyne Continental Motors | Teledyne Continental Motors IO-520-A,Teledyne Continental Motors IO-520-B,Teledyne Continental Motors IO-520-BA,Teledyne Continental Motors IO-520-BB,Teledyne Continental Motors IO-520-C,Teledyne Continental Motors IO-520-CB,Teledyne Continental Motors IO-520-D,Teledyne Continental Motors IO-520-E,Teledyne Continental Motors IO-520-F,Teledyne Continental Motors IO-520-J,Teledyne Continental Motors IO-520-K,Teledyne Continental Motors IO-520-L,Teledyne Continental Motors IO-520-M,Teledyne Continental Motors IO-520-MB,Teledyne Continental Motors IO-520-N,Teledyne Continental Motors IO-520-NB,Teledyne Continental Motors IO-550-A,Teledyne Continental Motors IO-550-B,Teledyne Continental Motors IO-550-C,Teledyne Continental Motors IO-550-D,Teledyne Continental Motors IO-550-E,Teledyne Continental Motors IO-550-F,Teledyne Continental Motors IO-550-G,Teledyne Continental Motors IO-550-L,Teledyne Continental Motors IO-550-N,Teledyne Continental Motors IO-550-P,Teledyne Continental Motors IO-550-R,Teledyne Continental Motors TSIO-520-A,Teledyne Continental Motors TSIO-520-AE,Teledyne Continental Motors TSIO-520-AF,Teledyne Continental Motors TSIO-520-B,Teledyne Continental Motors TSIO-520-BB,Teledyne Continental Motors TSIO-520-BE,Teledyne Continental Motors TSIO-520-C,Teledyne Continental Motors TSIO-520-CE,Teledyne Continental Motors TSIO-520-D,Teledyne Continental Motors TSIO-520-DB,Teledyne Continental Motors TSIO-520-E,Teledyne Continental Motors TSIO-520-EB,Teledyne Continental Motors TSIO-520-G,Teledyne Continental Motors TSIO-520-H,Teledyne Continental Motors TSIO-520-J,Teledyne Continental Motors TSIO-520-JB,Teledyne Continental Motors TSIO-520-K,Teledyne Continental Motors TSIO-520-KB,Teledyne Continental Motors TSIO-520-L,Teledyne Continental Motors TSIO-520-LB,Teledyne Continental Motors TSIO-520-M,Teledyne Continental Motors TSIO-520-N,Teledyne Continental Motors TSIO-520-NB,Teledyne Continental Motors TSIO-520-P,Teledyne Continental Motors TSIO-520-R,Teledyne Continental Motors TSIO-520-T,Teledyne Continental Motors TSIO-520-U,Teledyne Continental Motors TSIO-520-UB,Teledyne Continental Motors TSIO-520-VB,Teledyne Continental Motors TSIO-520-WB | IO-520-A,IO-520-B,IO-520-BA,IO-520-BB,IO-520-C,IO-520-CB,IO-520-D,IO-520-E,IO-520-F,IO-520-J,IO-520-K,IO-520-L,IO-520-M,IO-520-MB,IO-520-N,IO-520-NB,IO-550-A,IO-550-B,IO-550-C,IO-550-D,IO-550-E,IO-550-F,IO-550-G,IO-550-L,IO-550-N,IO-550-P,IO-550-R,TSIO-520-A,TSIO-520-AE,TSIO-520-AF,TSIO-520-B,TSIO-520-BB,TSIO-520-BE,TSIO-520-C,TSIO-520-CE,TSIO-520-D,TSIO-520-DB,TSIO-520-E,TSIO-520-EB,TSIO-520-G,TSIO-520-H,TSIO-520-J,TSIO-520-JB,TSIO-520-K,TSIO-520-KB,TSIO-520-L,TSIO-520-LB,TSIO-520-M,TSIO-520-N,TSIO-520-NB,TSIO-520-P,TSIO-520-R,TSIO-520-T,TSIO-520-U,TSIO-520-UB,TSIO-520-VB,TSIO-520-WB | Part 39 | Airworthiness Directives | 07/23/2009 | 1 | 2009-16-03.pdf | 40147 |
| 2009-16-02 | FAA-2009-0509 | 39-15985 | 09/09/2009 | 08/05/2009 | | | | Pilatus Aircraft Limited Model PC-7 Airplanes | Fuselage.
| Pilatus Aircraft Limited | Pilatus Aircraft Limited | Pilatus Aircraft Limited PC-7 | PC-7 | Part 39 | Airworthiness Directives | 07/23/2009 | 1 | 2009-16-02.pdf | 31806 |
| 2009-16-01 | FAA-2009-0463 | 39-15984 | 09/09/2009 | 08/05/2009 | | | | BAE Systems (Operations) Limited (Jetstream) Model
4101 Airplanes | Landing Gear
| BAE Systems (Operations) Limited | BAE Systems (Operations) Limited | BAE Systems (Operations) Limited Jetstream Model 4101 | Jetstream Model 4101 | Part 39 | Airworthiness Directives | 07/22/2009 | 1 | 2009-16-01.pdf | 34027 |
| 2009-15-19 | FAA-2009-0432 | 39-15982 | 09/02/2009 | 09/02/2009 | | | | BAE Systems (Operations) Limited Model BAe 146-100A
and 146-200A Series Airplanes | Stabilizers | BAE Systems (Operations) Limited | BAE Systems (Operations) Limited,BAE Systems (Operations) Limited | BAE Systems (Operations) Limited BAe 146-100A,BAE Systems (Operations) Limited BAe 146-200A | BAe 146-100A,BAe 146-200A | Part 39 | Airworthiness Directives | 07/13/2009 | 1 | 2009-15-19_Correction.pdf | 39925 |
| 2009-15-18 | FAA-2008-1005 | 39-15981 | 09/02/2009 | 07/29/2009 | | | | Empresa Brasileira de Aeronautica S.A. (EMBRAER)
Model EMB-120, -120ER, -120FC, -120QC, and -120RT Airplanes | Fuel
| Embraer - Empresa Brasileira de Aeronautica S.A. | Embraer - Empresa Brasileira de Aer,Embraer - Empresa Brasileira de Aer,Embraer - Empresa Brasileira de Aer,Embraer - Empresa Brasileira de Aer,Embraer - Empresa Brasileira de Aer | Embraer - Empresa Brasileira de Aeronautica S.A. EMB-120,Embraer - Empresa Brasileira de Aeronautica S.A. EMB-120ER,Embraer - Empresa Brasileira de Aeronautica S.A. EMB-120FC,Embraer - Empresa Brasileira de Aeronautica S.A. EMB-120QC,Embraer - Empresa Brasileira de Aeronautica S.A. EMB-120RT | EMB-120,EMB-120ER,EMB-120FC,EMB-120QC,EMB-120RT | Part 39 | Airworthiness Directives | 07/13/2009 | 1 | 2009-15-18.pdf | 36487 |
| 2009-15-17 | FAA-2009-0211 | 39-15980 | 09/02/2009 | 07/29/2009 | | | | Airbus Model A330-200, A330-300, A340- 200, and
A340-300 Series Airplanes | Landing gear
| Airbus | Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus | Airbus A330-201,Airbus A330-202,Airbus A330-203,Airbus A330-223,Airbus A330-243,Airbus A330-301,Airbus A330-302,Airbus A330-303,Airbus A330-321,Airbus A330-322,Airbus A330-323,Airbus A330-341,Airbus A330-342,Airbus A330-343,Airbus A340-211,Airbus A340-212,Airbus A340-213,Airbus A340-311,Airbus A340-312,Airbus A340-313 | A330-201,A330-202,A330-203,A330-223,A330-243,A330-301,A330-302,A330-303,A330-321,A330-322,A330-323,A330-341,A330-342,A330-343,A340-211,A340-212,A340-213,A340-311,A340-312,A340-313 | Part 39 | Airworthiness Directives | 07/02/2009 | 1 | 2009-15-17.pdf | 44970 |
| 2009-15-15 | FAA-2009-0227 | 39-15978 | 09/08/2009 | 08/03/2009 | | | | Bell Helicopter Textron Canada Model 427 Helicopters | Vertical Stabilizer, Attach Fittings | Bell Helicopter Textron (Canada) | Bell Helicopter Textron (Canada) | Bell Helicopter Textron (Canada) 427 | 427 | Part 39 | Airworthiness Directives | 07/14/2009 | 1 | 2009-15-15.pdf | 28532 |
| 2009-15-14 | FAA-2009-0168 | 39-15977 | 09/09/2009 | 08/05/2009 | | | | Agusta S.p.A. Model AB139 and AW139 Helicopters | Fire bottle, Fixed | Agusta S.p.A. | Agusta S.p.A.,Agusta S.p.A. | Agusta S.p.A. AB139,Agusta S.p.A. AW139 | AB139,AW139 | Part 39 | Airworthiness Directives | 07/10/2009 | 1 | 2009-15-14.pdf | 30385 |
| 2009-15-13 | FAA-2008-1311 | 39-15976 | 08/25/2009 | 07/21/2009 | | | | Honeywell International Inc., T5313 and T5317 Series
Turboshaft Engines | Combustion chamber housings (CCHs)
| Honeywell International Inc. | Honeywell International Inc.,Honeywell International Inc.,Honeywell International Inc.,Honeywell International Inc.,Honeywell International Inc. | Honeywell International Inc. T5313B,Honeywell International Inc. T5317A,Honeywell International Inc. T5317A-1,Honeywell International Inc. T5317B,Honeywell International Inc. T5317BCV | T5313B,T5317A,T5317A-1,T5317B,T5317BCV | Part 39 | Airworthiness Directives | 07/14/2009 | 1 | 2009-15-13.pdf | 57525 |
| 2009-15-12 | FAA-2007-28988 | 39-15975 | 08/25/2009 | 07/21/2009 | | | | Boeing Model 747-400 and -400D Series Airplanes | In-flight entertainment (IFE) system | Boeing Company^ The | Boeing Company, The,Boeing Company, The | Boeing Company^ The 747-400 Series,Boeing Company^ The 747-400D Series | 747-400 Series,747-400D Series | Part 39 | Airworthiness Directives | 07/06/2009 | 1 | 2009-15-12.pdf | 37037 |
| 2009-15-11 | FAA-2009-0646 | 39-15974 | 08/05/2009 | 07/21/2009 | | | | Aerospatiale Model SN-601 (Corvette) Airplanes | Landing gear | Aerospatiale (Societe Nationale Industrielle Aerospatiale) | Aerospatiale (Societe Nationale Ind | Aerospatiale (Societe Nationale Industrielle Aerospatiale) SN-601 Corvette | SN-601 Corvette | Part 39 | Airworthiness Directives | 07/02/2009 | 1 | 2009-15-11.pdf | 43357 |
| 2009-15-10 | FAA-2009-0645 | 39-15973 | 08/05/2009 | 07/21/2009 | | | | Airbus Model A330-301, -321, -322, - 341, and -342
Series Airplanes, and Airbus Model A340-211, -212, -213, -311, -312, and -313
Series Airplanes | Wings
| Airbus | Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus | Airbus A330-301,Airbus A330-321,Airbus A330-322,Airbus A330-341,Airbus A330-342,Airbus A340-211,Airbus A340-212,Airbus A340-213,Airbus A340-311,Airbus A340-312,Airbus A340-313 | A330-301,A330-321,A330-322,A330-341,A330-342,A340-211,A340-212,A340-213,A340-311,A340-312,A340-313 | Part 39 | Airworthiness Directives | 07/02/2009 | 1 | 2009-15-10.pdf | 37415 |
| 2009-15-09 | FAA-2009-0644 | 39-15972 | 08/05/2009 | 07/21/2009 | | | | Airbus Model A380-841, -842, and -861 Airplanes | Pneumatic | Airbus | Airbus,Airbus,Airbus | Airbus A380-841,Airbus A380-842,Airbus A380-861 | A380-841,A380-842,A380-861 | Part 39 | Airworthiness Directives | 07/06/2009 | 1 | 2009-15-09.pdf | 35417 |
| 2009-15-08 | FAA-2009-0398 | 39-15971 | 08/25/2009 | 07/21/2009 | | | | BAE Systems (Operations) Limited Model BAe 146 and
Avro 146-RJ Airplanes | Fuselage.
| BAE Systems (Operations) Limited | BAE Systems (Operations) Limited,BAE Systems (Operations) Limited,BAE Systems (Operations) Limited,BAE Systems (Operations) Limited,BAE Systems (Operations) Limited,BAE Systems (Operations) Limited | BAE Systems (Operations) Limited Avro 146-RJ100A,BAE Systems (Operations) Limited Avro 146-RJ70A,BAE Systems (Operations) Limited Avro 146-RJ85A,BAE Systems (Operations) Limited BAe 146-100A,BAE Systems (Operations) Limited BAe 146-200A,BAE Systems (Operations) Limited BAe 146-300A | Avro 146-RJ100A,Avro 146-RJ70A,Avro 146-RJ85A,BAe 146-100A,BAe 146-200A,BAe 146-300A | Part 39 | Airworthiness Directives | 07/02/2009 | 1 | 2009-15-08.pdf | 36779 |
| 2009-15-07 | FAA-2008-1365 | 39-15970 | 08/25/2009 | 07/21/2009 | | | | Airbus Model A319, A320, and A321 Series Airplanes | Landing gear
| Airbus | Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus | Airbus A318 Model -111,Airbus A318 Model -112,Airbus A319 Model -113,Airbus A319 Model -114,Airbus A319 Model -115,Airbus A319 Model -131,Airbus A319 Model -132,Airbus A319 Model -133,Airbus A320 Model -111,Airbus A320 Model -211,Airbus A320 Model -212,Airbus A320 Model -214,Airbus A320 Model -231,Airbus A320 Model -232,Airbus A320 Model -233,Airbus A321 Model-212,Airbus A321 Model-213,Airbus A321 Model-232,Airbus A321 Model -111,Airbus A321 Model -112,Airbus A321 Model -131,Airbus A321 Model -211,Airbus A321 Model -231 | A318 Model -111,A318 Model -112,A319 Model -113,A319 Model -114,A319 Model -115,A319 Model -131,A319 Model -132,A319 Model -133,A320 Model -111,A320 Model -211,A320 Model -212,A320 Model -214,A320 Model -231,A320 Model -232,A320 Model -233,A321 Model-212,A321 Model-213,A321 Model-232,A321 Model -111,A321 Model -112,A321 Model -131,A321 Model -211,A321 Model -231 | Part 39 | Airworthiness Directives | 07/02/2009 | 1 | 2009-15-07.pdf | 35112 |
| 2009-15-06 | FAA-2008-0645 | 39-15969 | 08/25/2009 | 07/21/2009 | | | | Boeing Model 707 Airplanes and Model 720 and 720B
Series Airplanes
| Fuel System
| Boeing Company^ The | Boeing Company, The,Boeing Company, The,Boeing Company, The,Boeing Company, The,Boeing Company, The,Boeing Company, The,Boeing Company, The,Boeing Company, The,Boeing Company, The,Boeing Company, The | Boeing Company^ The 707-100 Long Body,Boeing Company^ The 707-100B Long Body,Boeing Company^ The 707-100B Short Body,Boeing Company^ The 707-200,Boeing Company^ The 707-300 Series,Boeing Company^ The 707-300B Series,Boeing Company^ The 707-300C Series,Boeing Company^ The 707-400 Series,Boeing Company^ The 720 Series,Boeing Company^ The 720B Series | 707-100 Long Body,707-100B Long Body,707-100B Short Body,707-200,707-300 Series,707-300B Series,707-300C Series,707-400 Series,720 Series,720B Series | Part 39 | Airworthiness Directives | 07/02/2009 | 1 | 2009-15-06.pdf | 29511 |
| 2009-15-05 | FAA-2009-0638 | 39-15968 | 07/27/2009 | 07/15/2009 | | | | Cessna Aircraft Company Models 208 and 208B Airplanes | Yaw bridle cable tension | Cessna Aircraft Company | Cessna Aircraft Company,Cessna Aircraft Company | Cessna Aircraft Company 208,Cessna Aircraft Company 208B | 208,208B | Part 39 | Airworthiness Directives | 07/06/2009 | 1 | 2009-15-05.pdf | 34660 |
| 2009-15-04 | FAA-2009-0137 | 39-15967 | 08/19/2009 | 07/15/2009 | | | | Airbus Model A330-200 and -300, and A340-200 and -300
Series Airplanes | Electrical harness | Airbus | Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus | Airbus A330-201,Airbus A330-202,Airbus A330-203,Airbus A330-223,Airbus A330-243,Airbus A330-301,Airbus A330-302,Airbus A330-303,Airbus A330-321,Airbus A330-322,Airbus A330-323,Airbus A330-341,Airbus A330-342,Airbus A330-343,Airbus A340-211,Airbus A340-212,Airbus A340-213,Airbus A340-311,Airbus A340-312,Airbus A340-313 | A330-201,A330-202,A330-203,A330-223,A330-243,A330-301,A330-302,A330-303,A330-321,A330-322,A330-323,A330-341,A330-342,A330-343,A340-211,A340-212,A340-213,A340-311,A340-312,A340-313 | Part 39 | Airworthiness Directives | 07/02/2009 | 1 | 2009-15-04.pdf | 38177 |
| 2009-15-03 | FAA-2009-0138 | 39-15966 | 08/19/2009 | 07/15/2009 | 2008-24-12 | | | Bombardier Model BD-700-1A10 and BD- 700-1A11
Airplanes | Flight controls
| Bombardier Inc. | Bombardier Inc.,Bombardier Inc. | Bombardier Inc. BD-700-1A10,Bombardier Inc. BD-700-1A11 | BD-700-1A10,BD-700-1A11 | Part 39 | Airworthiness Directives | 07/02/2009 | 1 | 2009-15-03.pdf | 40892 |
| 2009-15-02 | FAA-2008-0832 | 39-15965 | 08/19/2009 | 07/15/2009 | | | | Airbus Model A318, A319, A320, and A321 Airplanes | Hydraulic power
| Airbus | Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus | Airbus A318 Model -111,Airbus A318 Model -112,Airbus A318 Model -121,Airbus A318 Model -122,Airbus A319 Model -111,Airbus A319 Model -112,Airbus A319 Model -113,Airbus A319 Model -114,Airbus A319 Model -115,Airbus A319 Model -131,Airbus A319 Model -132,Airbus A319 Model -133,Airbus A320 Model -111,Airbus A320 Model -211,Airbus A320 Model -212,Airbus A320 Model -214,Airbus A320 Model -231,Airbus A320 Model -232,Airbus A320 Model -233,Airbus A321 Model-212,Airbus A321 Model-213,Airbus A321 Model-232,Airbus A321 Model -111,Airbus A321 Model -112,Airbus A321 Model -131,Airbus A321 Model -211,Airbus A321 Model -231 | A318 Model -111,A318 Model -112,A318 Model -121,A318 Model -122,A319 Model -111,A319 Model -112,A319 Model -113,A319 Model -114,A319 Model -115,A319 Model -131,A319 Model -132,A319 Model -133,A320 Model -111,A320 Model -211,A320 Model -212,A320 Model -214,A320 Model -231,A320 Model -232,A320 Model -233,A321 Model-212,A321 Model-213,A321 Model-232,A321 Model -111,A321 Model -112,A321 Model -131,A321 Model -211,A321 Model -231 | Part 39 | Airworthiness Directives | 07/02/2009 | 1 | 2009-15-02.pdf | 35880 |
| 2009-15-01 | FAA-2009-0633 | 39-15964 | 07/27/2009 | 07/15/2009 | | | | Hawker Beechcraft Corporation (Type Certificate
Previously Held by Raytheon Aircraft Company) Model G36 Airplanes | Wire harness/connector(s)
| Hawker Beechcraft Corporation | Hawker Beechcraft Corporation | Hawker Beechcraft Corporation G36 | G36 | Part 39 | Airworthiness Directives | 07/02/2009 | 1 | 2009-15-01.pdf | 31754 |
| 2009-14-13 | FAA-2009-0437 | 39-15963 | 08/19/2009 | 07/15/2009 | 2003-14-07 | | | Pilatus Aircraft Ltd. Models PC-12, PC- 12/45,
PC-12/47, and PC-12/47E Airplanes | Landing gear
| Pilatus Aircraft Limited | Pilatus Aircraft Limited,Pilatus Aircraft Limited,Pilatus Aircraft Limited,Pilatus Aircraft Limited | Pilatus Aircraft Limited PC-12,Pilatus Aircraft Limited PC-12/45,Pilatus Aircraft Limited PC-12/47,Pilatus Aircraft Limited PC-12/47E | PC-12,PC-12/45,PC-12/47,PC-12/47E | Part 39 | Airworthiness Directives | 07/01/2009 | 1 | 2009-14-13.pdf | 38618 |
| 2009-14-12 | FAA-2009-0046 | 39-15962 | 08/13/2009 | 07/09/2009 | | | | Pratt & Whitney Canada Corp. (P&WC) Models PW305A and
PW305B Turbofan Engines | High Pressure Compressor (HPC)
| Pratt & Whitney Canada Corp. | Pratt & Whitney Canada Corp.,Pratt & Whitney Canada Corp. | Pratt & Whitney Canada Corp. PW305A,Pratt & Whitney Canada Corp. PW305B | PW305A,PW305B | Part 39 | Airworthiness Directives | 06/30/2009 | 1 | 2009-14-12.pdf | 28738 |
| 2009-14-11 | FAA-2009-0330 | 39-15961 | 08/19/2009 | 07/15/2009 | | | | Turbomeca S.A. ARRIUS 2F Turboshaft Engines | P3 air pipe
| Turbomeca S.A. | Turbomeca S.A. | Turbomeca S.A. Arrius 2F | Arrius 2F | Part 39 | Airworthiness Directives | 06/30/2009 | 1 | 2009-14-11.pdf | 28766 |
| 2009-14-10 | FAA-2009-0446 | 39-15960 | 08/12/2009 | 07/08/2009 | 2009-09-04 | | | EADS-PZL "Warszawa-Okecie'' S.A. Model PZL-104 WILGA
80 Airplanes | Fuselage
| EADS-PZL Warszawa-Okecie S.A. | EADS-PZL Warszawa-Okecie S.A. | EADS-PZL Warszawa-Okecie S.A. PZL-104 WILGA 80 | PZL-104 WILGA 80 | Part 39 | Airworthiness Directives | 06/30/2009 | 1 | 2009-14-10.pdf | 144402 |
| 2009-14-09 | FAA-2009-0380 | 39-15959 | 08/12/2009 | 07/08/2009 | | | | Dassault Model Falcon 2000EX Airplanes | Fuselage
| Dassault Aviation | Dassault Aviation | Dassault Aviation FALCON 2000EX | FALCON 2000EX | Part 39 | Airworthiness Directives | 06/25/2009 | 1 | 2009-14-09.pdf | 32734 |
| 2009-14-08 | FAA-2009-0121 | 39-15958 | 08/05/2009 | 07/01/2009 | | | | General Electric Company (GE) CF6- 80C2B5F Turbofan
Engines | High-pressure compressor rotor (HPCR) stages 11-14 spool/ shafts
| General Electric Company | General Electric Aircraft Engines | General Electric Company CF6-80C2B5F | CF6-80C2B5F | Part 39 | Airworthiness Directives | 06/25/2009 | 1 | 2009-14-08.pdf | 26716 |
| 2009-14-07 | FAA-2009-0263 | 39-15957 | 08/12/2009 | 07/08/2009 | | | | Dassault Model Mystere-Falcon 20-C5, 20-D5, 20-E5,
and 20-F5 Airplanes | Ice and rain protection
| Dassault Aviation | Dassault Aviation,Dassault Aviation,Dassault Aviation,Dassault Aviation | Dassault Aviation Mystere-Falcon 20 - C5,Dassault Aviation Mystere-Falcon 20 - D5,Dassault Aviation Mystere-Falcon 20 - E5,Dassault Aviation Mystere-Falcon 20 - F5 | Mystere-Falcon 20 - C5,Mystere-Falcon 20 - D5,Mystere-Falcon 20 - E5,Mystere-Falcon 20 - F5 | Part 39 | Airworthiness Directives | 06/24/2009 | 1 | 2009-14-07.pdf | 32264 |
| 2009-14-06 | FAA-2008-0933 | 39-15956 | 08/12/2009 | 07/08/2009 | 2007-17-12 | | | Boeing Model 777 Airplanes | Horizontal stabilizer | Boeing Company^ The | Boeing Company, The,Boeing Company, The,Boeing Company, The,Boeing Company, The,Boeing Company, The | Boeing Company^ The 777-200 Series,Boeing Company^ The 777-200LR,Boeing Company^ The 777-300 Series,Boeing Company^ The 777-300ER Series,Boeing Company^ The 777F | 777-200 Series,777-200LR,777-300 Series,777-300ER Series,777F | Part 39 | Airworthiness Directives | 06/24/2009 | 1 | 2009-14-06.pdf | 39201 |
| 2009-14-05 | FAA-2009-0417 | 39-15955 | 07/23/2009 | 07/08/2009 | | | | Pratt & Whitney Models PW2037, PW2037(M), and PW2040
Turbofan Engines | High-pressure compressor (HPC) | Pratt & Whitney Division | Pratt & Whitney Division,Pratt & Whitney Division,Pratt & Whitney Division | Pratt & Whitney Division PW2037,Pratt & Whitney Division PW2037M,Pratt & Whitney Division PW2040 | PW2037,PW2037M,PW2040 | Part 39 | Airworthiness Directives | 06/23/2009 | 1 | 2009-14-05.pdf | 32519 |
| 2009-14-04 | FAA-2008-1116 | 39-15954 | 08/12/2009 | 07/08/2009 | | | | Boeing Model 737-100, -200, -200C, - 300, -400, and
-500 Series Airplanes | Outboard landing lights | Boeing Company^ The | Boeing Company, The,Boeing Company, The,Boeing Company, The,Boeing Company, The,Boeing Company, The,Boeing Company, The | Boeing Company^ The 737-100 Series,Boeing Company^ The 737-200 Series,Boeing Company^ The 737-200C Series,Boeing Company^ The 737-300 Series,Boeing Company^ The 737-400 Series,Boeing Company^ The 737-500 Series | 737-100 Series,737-200 Series,737-200C Series,737-300 Series,737-400 Series,737-500 Series | Part 39 | Airworthiness Directives | 06/11/2009 | 1 | 2009-14-04.pdf | 37330 |
| 2009-14-03 | FAA-2009-0044 | 39-15953 | 08/12/2009 | 07/08/2009 | | | | Bombardier Model CL-600-1A11 (CL-600), CL-600-2A12
(CL-601), CL-600-2B16 (CL-601-3A, CL-601-3R, and CL-604) Airplanes | Flight Controls
| Bombardier Inc. | Bombardier Inc.,Bombardier Inc.,Bombardier Inc.,Bombardier Inc.,Bombardier Inc. | Bombardier Inc. CL-600-1A11 (CL-600),Bombardier Inc. CL-600-2A12 (CL-601),Bombardier Inc. CL-600-2B16 (CL-601-3A),Bombardier Inc. CL-600-2B16 (CL-601-3R),Bombardier Inc. CL-600-2B16 (CL-604) | CL-600-1A11 (CL-600),CL-600-2A12 (CL-601),CL-600-2B16 (CL-601-3A),CL-600-2B16 (CL-601-3R),CL-600-2B16 (CL-604) | Part 39 | Airworthiness Directives | 06/11/2009 | 1 | 2009-14-03.pdf | 37689 |
| 2009-14-02 | FAA-2008-1071 | 39-15951 | 08/03/2009 | 06/29/2009 | 2002-26-15 | | | Boeing Model 747 Airplanes | Vertical stabilizer seal and fuselage skin | Boeing Company^ The | Boeing Company, The,Boeing Company, The,Boeing Company, The,Boeing Company, The,Boeing Company, The,Boeing Company, The,Boeing Company, The,Boeing Company, The,Boeing Company, The,Boeing Company, The,Boeing Company, The,Boeing Company, The | Boeing Company^ The 747-100 Series,Boeing Company^ The 747-100B Series,Boeing Company^ The 747-100B SUD Series,Boeing Company^ The 747-200B Series,Boeing Company^ The 747-200C Series,Boeing Company^ The 747-200F Series,Boeing Company^ The 747-300 Series,Boeing Company^ The 747-400 Series,Boeing Company^ The 747-400D Series,Boeing Company^ The 747-400F Series,Boeing Company^ The 747SP Series,Boeing Company^ The 747SR Series | 747-100 Series,747-100B Series,747-100B SUD Series,747-200B Series,747-200C Series,747-200F Series,747-300 Series,747-400 Series,747-400D Series,747-400F Series,747SP Series,747SR Series | Part 39 | Airworthiness Directives | 06/19/2009 | 1 | 2009-14-02.pdf | 43189 |
| 2009-14-01 | FAA-2005-22039 | 39-15950 | 08/03/2009 | 06/29/2009 | 2005-17-17R1 | | | Turbomeca S.A. Arrius 2F Turboshaft Engines | Check valve piston
| Turbomeca S.A. | Turbomeca S.A. | Turbomeca S.A. Arrius 2F | Arrius 2F | Part 39 | Airworthiness Directives | 06/19/2009 | 1 | 2009-14-01.pdf | 30612 |
| 2009-13-10 | FAA-2009-0570 | 39-15949 | 06/26/2009 | 06/24/2009 | | 2009-19-03 | | British Aerospace Regional Aircraft Model HP.137
Jetstream Mk.1, Jetstream Series 200 and 3101, and Jetstream Model 3201
Airplanes | Landing gear
| British Aerospace Regional Aircraft | British Aerospace (Scotland),British Aerospace (Scotland),British Aerospace (Scotland),British Aerospace (Scotland) | British Aerospace Regional Aircraft H.P. 137 Jetstream Mk. 1,British Aerospace Regional Aircraft Jetstream 3201,British Aerospace Regional Aircraft Jetstream Series 200,British Aerospace Regional Aircraft Jetstream Series 3101 | H.P. 137 Jetstream Mk. 1,Jetstream 3201,Jetstream Series 200,Jetstream Series 3101 | Part 39 | Airworthiness Directives | 06/18/2009 | 1 | 2009-13-10.pdf | 36308 |
| 2009-13-09 | FAA-2009-0510 | 39-15948 | 07/14/2009 | 06/29/2009 | | | | Microturbo SA Saphir 2 Model 016 Auxiliary Power
Units | Auxiliary Power Units | Dassault Aviation | Dassault Aviation,Dassault Aviation,Dassault Aviation,Dassault Aviation | Dassault Aviation Mystere-Falcon 20 - C5,Dassault Aviation Mystere-Falcon 20 - D5,Dassault Aviation Mystere-Falcon 20 - E5,Dassault Aviation Mystere-Falcon 20 - F5 | Mystere-Falcon 20 - C5,Mystere-Falcon 20 - D5,Mystere-Falcon 20 - E5,Mystere-Falcon 20 - F5 | Part 39 | Airworthiness Directives | 06/17/2009 | 1 | 2009-13-09.pdf | 32441 |
| 2009-13-08 | FAA-2009-0160 | 39-15947 | 08/03/2009 | 06/29/2009 | | | | McDonnell Douglas Model MD-90-30 Airplanes | Stabilizers
| McDonnell Douglas Corporation | McDonnell Douglas Corporation | McDonnell Douglas Corporation MD-90-30 | MD-90-30 | Part 39 | Airworthiness Directives | 06/16/2009 | 1 | 2009-13-08.pdf | 29798 |
| 2009-13-07 | FAA-2009-0262 | 39-15946 | 07/24/2009 | 06/19/2009 | | | | Airbus Model A330-201, -202, -203, - 223, -243, -301,
-302, -303, -321, -322, -323, -341, -342, and -343 Series Airplanes | Fire protection
| Airbus | Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus | Airbus A330-201,Airbus A330-202,Airbus A330-203,Airbus A330-223,Airbus A330-243,Airbus A330-301,Airbus A330-302,Airbus A330-303,Airbus A330-321,Airbus A330-322,Airbus A330-323,Airbus A330-341,Airbus A330-342,Airbus A330-343 | A330-201,A330-202,A330-203,A330-223,A330-243,A330-301,A330-302,A330-303,A330-321,A330-322,A330-323,A330-341,A330-342,A330-343 | Part 39 | Airworthiness Directives | 06/11/2009 | 1 | 2009-13-07.pdf | 33711 |
| 2009-13-06 | FAA-2009-0218 | 39-15944 | 07/24/2009 | 06/19/2009 | | | | Piper Aircraft, Inc. PA-23, PA-31, and PA-42 Series
Airplanes | Nose baggage door | Piper Aircraft^ Inc. | Piper Aircraft, Inc.,Piper Aircraft, Inc.,Piper Aircraft, Inc.,Piper Aircraft, Inc.,Piper Aircraft, Inc.,Piper Aircraft, Inc.,Piper Aircraft, Inc.,Piper Aircraft, Inc.,Piper Aircraft, Inc.,Piper Aircraft, Inc.,Piper Aircraft, Inc.,Piper Aircraft, Inc.,Piper Aircraft, Inc.,Piper Aircraft, Inc.,Piper Aircraft, Inc.,Piper Aircraft, Inc.,Piper Aircraft, Inc. | Piper Aircraft^ Inc. PA-23,Piper Aircraft^ Inc. PA-23-160,Piper Aircraft^ Inc. PA-23-235,Piper Aircraft^ Inc. PA-23-250 (Navy UO-1),Piper Aircraft^ Inc. PA-31,Piper Aircraft^ Inc. PA-31-300,Piper Aircraft^ Inc. PA-31-325,Piper Aircraft^ Inc. PA-31-350,Piper Aircraft^ Inc. PA-31P,Piper Aircraft^ Inc. PA-31P-350,Piper Aircraft^ Inc. PA-31T,Piper Aircraft^ Inc. PA-31T1,Piper Aircraft^ Inc. PA-31T2,Piper Aircraft^ Inc. PA-31T3,Piper Aircraft^ Inc. PA-42,Piper Aircraft^ Inc. PA-42-1000,Piper Aircraft^ Inc. PA-42-720 | PA-23,PA-23-160,PA-23-235,PA-23-250 (Navy UO-1),PA-31,PA-31-300,PA-31-325,PA-31-350,PA-31P,PA-31P-350,PA-31T,PA-31T1,PA-31T2,PA-31T3,PA-42,PA-42-1000,PA-42-720 | Part 39 | Airworthiness Directives | 06/12/2009 | 1 | 2009-13-06.pdf | 35414 |
| 2009-13-05 | FAA-2009-0557 | 39-15944 | 07/09/2009 | 06/19/2009 | | | | SOCATA Model TBM 700 Airplanes | Oxygen
| SOCATA | SOCATA | SOCATA TBM 700 | TBM 700 | Part 39 | Airworthiness Directives | 06/10/2009 | 1 | 2009-13-05.pdf | 34486 |
| 2009-13-04 | FAA-2009-0261 | 39-15943 | 07/24/2009 | 06/19/2009 | | | | Dornier Luftfahrt GmbH Models Dornier 228-100,
Dornier 228-101, Dornier 228-200, Dornier 228-201, Dornier 228-202, and Dornier
228-212 Airplanes | Engine controls
| Dornier Luftfahrt GmbH | Dornier Luftfahrt GmbH,Dornier Luftfahrt GmbH,Dornier Luftfahrt GmbH,Dornier Luftfahrt GmbH,Dornier Luftfahrt GmbH,Dornier Luftfahrt GmbH | Dornier Luftfahrt GmbH Dornier 228-100,Dornier Luftfahrt GmbH Dornier 228-101,Dornier Luftfahrt GmbH Dornier 228-200,Dornier Luftfahrt GmbH Dornier 228-201,Dornier Luftfahrt GmbH Dornier 228-202,Dornier Luftfahrt GmbH Dornier 228-212 | Dornier 228-100,Dornier 228-101,Dornier 228-200,Dornier 228-201,Dornier 228-202,Dornier 228-212 | Part 39 | Airworthiness Directives | 06/10/2009 | 1 | 2009-13-04.pdf | 31355 |
| 2009-13-03 | FAA-2009-0556 | 39-15942 | 07/06/2009 | 06/30/2009 | | | | Boeing Model 747-400 and -400F Series Airplanes
Powered by Rolls-Royce RB211 Series Engines | Engine | Boeing Company^ The | Boeing Company, The,Boeing Company, The | Boeing Company^ The 747-400 Series,Boeing Company^ The 747-400F Series | 747-400 Series,747-400F Series | Part 39 | Airworthiness Directives | 06/12/2009 | 1 | 2009-13-03.pdf | 33728 |
| 2009-13-02 | FAA-2009-0198 | 39-15941 | 08/03/2009 | 06/29/2009 | 98-06-07 | | | Fokker Model F.28 Mark 0100 Airplanes | Engine controls
| Fokker Services | Fokker Services | Fokker Services F.28 Mark 0100 | F.28 Mark 0100 | Part 39 | Airworthiness Directives | 06/16/2009 | 1 | 2009-13-02.pdf | 33580 |
| 2009-13-01 | FAA-2009-0518 | 39-15940 | 04/27/2009 | 06/16/2009 | 2009-07-53
2009-07-53 | | | Sikorsky Aircraft Corporation Model S- 92A
Helicopters | Main gearbox (MGB) filter bowl assembly
| Sikorsky Aircraft Corporation | Sikorsky Aircraft Corporation | Sikorsky Aircraft Corporation S-92A | S-92A | Part 39 | Airworthiness Directives | 06/09/2009 | 1 | 2009-13-01.pdf | 35398 |
| 2009-12-51 | Unknown | | | | | | | Emergency AD: Airworthiness Directives: Turbomeca S.A. Arriel 1A1, 1A2, 1B, 1C, 1C1, 1C2, 1D,
1D1, 1E2, 1K1, 1S, and 1S1 turboshaft engine | Gearbox | Turbomeca S.A. | Turbomeca S.A.,Turbomeca S.A.,Turbomeca S.A.,Turbomeca S.A.,Turbomeca S.A.,Turbomeca S.A.,Turbomeca S.A.,Turbomeca S.A.,Turbomeca S.A.,Turbomeca S.A.,Turbomeca S.A.,Turbomeca S.A. | Turbomeca S.A. Arriel 1A1,Turbomeca S.A. Arriel 1A2,Turbomeca S.A. Arriel 1B,Turbomeca S.A. Arriel 1C,Turbomeca S.A. Arriel 1C1,Turbomeca S.A. Arriel 1C2,Turbomeca S.A. Arriel 1D,Turbomeca S.A. Arriel 1D1,Turbomeca S.A. Arriel 1E2,Turbomeca S.A. Arriel 1K1,Turbomeca S.A. Arriel 1S,Turbomeca S.A. Arriel 1S1 | Arriel 1A1,Arriel 1A2,Arriel 1B,Arriel 1C,Arriel 1C1,Arriel 1C2,Arriel 1D,Arriel 1D1,Arriel 1E2,Arriel 1K1,Arriel 1S,Arriel 1S1 | Part 39 | Emergency AD | 06/04/2009 | 1 | 2009-12-51_Emergency.pdf | 25438 |
| 2009-12-16 | FAA-2009-0284 | 39-15939 | 07/17/2009 | 06/12/2009 | 2008-08-15 | | | Dornier Luftfahrt GmbH Models Dornier 228-100,
Dornier 228-101, Dornier 228-200, Dornier 228-201, Dornier 228-202, and Dornier
228-212 Airplanes | Standard Practices/Structures
| Dornier Luftfahrt GmbH | Dornier Luftfahrt GmbH,Dornier Luftfahrt GmbH,Dornier Luftfahrt GmbH,Dornier Luftfahrt GmbH,Dornier Luftfahrt GmbH,Dornier Luftfahrt GmbH | Dornier Luftfahrt GmbH Dornier 228-100,Dornier Luftfahrt GmbH Dornier 228-101,Dornier Luftfahrt GmbH Dornier 228-200,Dornier Luftfahrt GmbH Dornier 228-201,Dornier Luftfahrt GmbH Dornier 228-202,Dornier Luftfahrt GmbH Dornier 228-212 | Dornier 228-100,Dornier 228-101,Dornier 228-200,Dornier 228-201,Dornier 228-202,Dornier 228-212 | Part 39 | Airworthiness Directives | 06/04/2009 | 1 | 2009-12-16.pdf | 33799 |
| 2009-12-15 | FAA-2009-0531 | 39-15938 | 07/01/2009 | 06/11/2009 | | | | GROB-Werke Model G120A Airplanes | Electric Power
| Grob-Werke | Grob-Werke | Grob-Werke G120A | G120A | Part 39 | Airworthiness Directives | 06/04/2009 | 1 | 2009-12-15.pdf | 34434 |
| 2009-12-14 | FAA-2009-0323 | 39-15937 | 07/17/2009 | 06/12/2009 | | | | Aeromot-Industria Mecanico Metalurgica ltda. Model
AMT-200 and AMT-300 Series Gliders | Engine fuel & control
| Aeromot-Industria Mecanico Metalurgica Ltda. | Aeromot-Industria Mecanico Metalurg,Aeromot-Industria Mecanico Metalurg,Aeromot-Industria Mecanico Metalurg,Aeromot-Industria Mecanico Metalurg | Aeromot-Industria Mecanico Metalurgica Ltda. AMT-100 (Ximango),Aeromot-Industria Mecanico Metalurgica Ltda. AMT-200 (Super Ximango),Aeromot-Industria Mecanico Metalurgica Ltda. AMT-200S (Super Ximango),Aeromot-Industria Mecanico Metalurgica Ltda. AMT-300 (Turbo Ximango Shark) | AMT-100 (Ximango),AMT-200 (Super Ximango),AMT-200S (Super Ximango),AMT-300 (Turbo Ximango Shark) | Part 39 | Airworthiness Directives | 06/04/2009 | 1 | 2009-12-14.pdf | 32234 |
| 2009-12-13 | FAA-2009-0530 | 39-15936 | 06/26/2009 | 06/11/2009 | | | | Bombardier Model DHC-8-400 Series Airplanes | Flight Controls | Bombardier Inc. | Bombardier Inc. | Bombardier Inc. DHC-8-400 Series | DHC-8-400 Series | Part 39 | Airworthiness Directives | 06/03/2009 | 1 | 2009-12-13.pdf | 36662 |
| 2009-12-12 | FAA-2009-0524 | 39-15935 | 06/29/2009 | 06/12/2009 | | | | ATR Model ATR42-500 and ATR72-212A Airplanes | Electrical power
| ATR – GIE Avions de Transport Régional | ATR – GIE Avions de Transport Régio,ATR – GIE Avions de Transport Régio | ATR – GIE Avions de Transport Régional ATR42-500,ATR – GIE Avions de Transport Régional ATR72-212A | ATR42-500,ATR72-212A | Part 39 | Airworthiness Directives | 06/02/2009 | 1 | 2009-12-12.pdf | 35054 |
| 2009-12-11 | FAA-2009-0523 | 39-15934 | 06/29/2009 | 06/12/2009 | | | | Airbus Model A340-541 and -642 Airplanes | Fuselage
| Airbus | Airbus,Airbus | Airbus A340-541,Airbus A340-642 | A340-541,A340-642 | Part 39 | Airworthiness Directives | 06/02/2009 | 1 | 2009-12-11.pdf | 34448 |
| 2009-12-10 | FAA-2009-0133 | 39-15933 | 07/24/2009 | 06/19/2009 | 2006-12-09 | | | BAE Systems (Operations) Limited Model BAe 146 and
Avro 146-RJ Airplanes | Fuselage
| BAE Systems (Operations) Limited | BAE Systems (Operations) Limited,BAE Systems (Operations) Limited,BAE Systems (Operations) Limited,BAE Systems (Operations) Limited,BAE Systems (Operations) Limited,BAE Systems (Operations) Limited | BAE Systems (Operations) Limited Avro 146-RJ100A,BAE Systems (Operations) Limited Avro 146-RJ70A,BAE Systems (Operations) Limited Avro 146-RJ85A,BAE Systems (Operations) Limited BAe 146-100A,BAE Systems (Operations) Limited BAe 146-200A,BAE Systems (Operations) Limited BAe 146-300A | Avro 146-RJ100A,Avro 146-RJ70A,Avro 146-RJ85A,BAe 146-100A,BAe 146-200A,BAe 146-300A | Part 39 | Airworthiness Directives | 06/02/2009 | 1 | 2009-12-10.pdf | 34346 |
| 2009-12-09 | FAA-2008-1237 | 39-15932 | 07/16/2009 | 06/11/2009 | | | | ATR Model ATR42-200, ATR42-300, ATR42- 320,
ATR42-500, ATR72-101, ATR72-201, ATR72-102, ATR72-202, ATR72-211, ATR72-212,
and ATR72-212A Airplanes | Electrical power
| ATR – GIE Avions de Transport Régional | ATR – GIE Avions de Transport Régio,ATR – GIE Avions de Transport Régio,ATR – GIE Avions de Transport Régio,ATR – GIE Avions de Transport Régio,ATR – GIE Avions de Transport Régio,ATR – GIE Avions de Transport Régio,ATR – GIE Avions de Transport Régio,ATR – GIE Avions de Transport Régio,ATR – GIE Avions de Transport Régio,ATR – GIE Avions de Transport Régio,ATR – GIE Avions de Transport Régio | ATR – GIE Avions de Transport Régional ATR42-200,ATR – GIE Avions de Transport Régional ATR42-300,ATR – GIE Avions de Transport Régional ATR42-320,ATR – GIE Avions de Transport Régional ATR42-500,ATR – GIE Avions de Transport Régional ATR72-101,ATR – GIE Avions de Transport Régional ATR72-102,ATR – GIE Avions de Transport Régional ATR72-201,ATR – GIE Avions de Transport Régional ATR72-202,ATR – GIE Avions de Transport Régional ATR72-211,ATR – GIE Avions de Transport Régional ATR72-212,ATR – GIE Avions de Transport Régional ATR72-212A | ATR42-200,ATR42-300,ATR42-320,ATR42-500,ATR72-101,ATR72-102,ATR72-201,ATR72-202,ATR72-211,ATR72-212,ATR72-212A | Part 39 | Airworthiness Directives | 06/02/2009 | 1 | 2009-12-09.pdf | 37674 |
| 2009-12-08 | FAA-2008-0612 | 39-15931 | 07/16/2009 | 06/11/2009 | | | | Boeing Model 747 Airplanes | Fuselage | Boeing Company^ The | Boeing Company, The,Boeing Company, The,Boeing Company, The,Boeing Company, The,Boeing Company, The,Boeing Company, The,Boeing Company, The,Boeing Company, The,Boeing Company, The,Boeing Company, The,Boeing Company, The,Boeing Company, The | Boeing Company^ The 747-100 Series,Boeing Company^ The 747-100B Series,Boeing Company^ The 747-100B SUD Series,Boeing Company^ The 747-200B Series,Boeing Company^ The 747-200C Series,Boeing Company^ The 747-200F Series,Boeing Company^ The 747-300 Series,Boeing Company^ The 747-400 Series,Boeing Company^ The 747-400D Series,Boeing Company^ The 747-400F Series,Boeing Company^ The 747SP Series,Boeing Company^ The 747SR Series | 747-100 Series,747-100B Series,747-100B SUD Series,747-200B Series,747-200C Series,747-200F Series,747-300 Series,747-400 Series,747-400D Series,747-400F Series,747SP Series,747SR Series | Part 39 | Airworthiness Directives | 06/02/2009 | 1 | 2009-12-08.pdf | 31007 |
| 2009-12-07 | FAA-2009-0226 | 39-15930 | 07/17/2009 | 06/12/2009 | | | | Agusta S.p.A. Model A109E, A109S, A119, and AW119MKII
Helicopters | Cargo hook lever | Agusta S.p.A. | Agusta S.p.A.,Agusta S.p.A.,Agusta S.p.A. | Agusta S.p.A. A109S,Agusta S.p.A. A119,Agusta S.p.A. AW119 MKII | A109S,A119,AW119 MKII | Part 39 | Airworthiness Directives | 05/21/2009 | 1 | 2009-12-07.pdf | 30198 |
| 2009-12-06 | FAA-2007-0163 | 39-15929 | 07/16/2009 | 06/11/2009 | | | | Boeing Model 737-300, -400, -500, -600, -700, -700C,
-800, and -900 Series Airplanes | Circuit breaker | Boeing Company^ The | Boeing Company, The,Boeing Company, The,Boeing Company, The,Boeing Company, The,Boeing Company, The,Boeing Company, The,Boeing Company, The,Boeing Company, The | Boeing Company^ The 737-300 Series,Boeing Company^ The 737-400 Series,Boeing Company^ The 737-500 Series,Boeing Company^ The 737-600 Series,Boeing Company^ The 737-700 Series,Boeing Company^ The 737-700C Series,Boeing Company^ The 737-800 Series,Boeing Company^ The 737-900 Series | 737-300 Series,737-400 Series,737-500 Series,737-600 Series,737-700 Series,737-700C Series,737-800 Series,737-900 Series | Part 39 | Airworthiness Directives | 06/01/2009 | 1 | 2009-12-06.pdf | 42779 |
| 2009-12-05 | FAA-2008-1364 | 39-15928 | 07/16/2009 | 06/11/2009 | | | | Boeing Model 737-300, -400, and -500 Series Airplanes | Electronic flight instrument system (EFIS)
| Boeing Company^ The | Boeing Company, The,Boeing Company, The,Boeing Company, The | Boeing Company^ The 737-300 Series,Boeing Company^ The 737-400 Series,Boeing Company^ The 737-500 Series | 737-300 Series,737-400 Series,737-500 Series | Part 39 | Airworthiness Directives | 06/01/2009 | 1 | 2009-12-05.pdf | 31962 |
| 2009-12-04 | FAA-2009-0005 | 39-15927 | 07/16/2009 | 06/11/2009 | | | | Construcciones Aeronauticas, S.A. (CASA), Model
C-212-CB, C-212-CC, C-212-CD, C-212-CE, C-212-CF, and C- 212-DE Airplanes | Navigation
| Construcciones Aeronauticas^ S.A. | Construcciones Aeronauticas, S.A.,Construcciones Aeronauticas, S.A.,Construcciones Aeronauticas, S.A.,Construcciones Aeronauticas, S.A.,Construcciones Aeronauticas, S.A.,Construcciones Aeronauticas, S.A. | Construcciones Aeronauticas^ S.A. C-212-CB,Construcciones Aeronauticas^ S.A. C-212-CC,Construcciones Aeronauticas^ S.A. C-212-CD,Construcciones Aeronauticas^ S.A. C-212-CE,Construcciones Aeronauticas^ S.A. C-212-CF,Construcciones Aeronauticas^ S.A. C-212-DE | C-212-CB,C-212-CC,C-212-CD,C-212-CE,C-212-CF,C-212-DE | Part 39 | Airworthiness Directives | 06/01/2009 | 1 | 2009-12-04.pdf | 34979 |
| 2009-12-03 | FAA-2007-29067 | 39-15926 | 07/16/2009 | 06/11/2009 | | | | Boeing Model 757-200, -200CB, and -300 Series
Airplanes | Right recirculation fan | Boeing Company^ The | Boeing Company, The,Boeing Company, The,Boeing Company, The | Boeing Company^ The 757-200 Series,Boeing Company^ The 757-200CB Series,Boeing Company^ The 757-300 Series | 757-200 Series,757-200CB Series,757-300 Series | Part 39 | Airworthiness Directives | 06/01/2009 | 1 | 2009-12-03.pdf | 31861 |
| 2009-12-02 | FAA-2008-1082 | 39-15925 | 07/24/2009 | 06/19/2009 | 2007-03-09 | | | Airbus Model A300 Airplanes; Model A300 B4-601,
B4-603, B4-620, B4-622, B4-605R, B4-622R, F4-605R, F4-622R, and C4-605R Variant
F Airplanes (Collectively Called A300-600 Series Airplanes); and Model A310
Airplanes | Ram air turbine (RAT)
| Airbus | Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus | Airbus A300B4-601,Airbus A300B4-603,Airbus A300B4-605R,Airbus A300B4-620,Airbus A300B4-622R,Airbus A300F4-605R,Airbus A300F4-622R,Airbus A300^ Model C4-605 Variant F,Airbus A310-203,Airbus A310-204,Airbus A310-221,Airbus A310-222,Airbus A310-304,Airbus A310-322,Airbus A310-324,Airbus A310-325 | A300B4-601,A300B4-603,A300B4-605R,A300B4-620,A300B4-622R,A300F4-605R,A300F4-622R,A300, Model C4-605 Variant F,A310-203,A310-204,A310-221,A310-222,A310-304,A310-322,A310-324,A310-325 | Part 39 | Airworthiness Directives | 05/20/2009 | 1 | 2009-12-02.pdf | 42988 |
| 2009-12-01 | FAA-2009-0484 | 39-15924 | 06/29/2009 | 06/12/2009 | | | | Bell Helicopter Textron, Inc. Model 47, 47B, 47B3,
47D, 47D1, 47E, 47G, 47G-2, 47G-2A, 47G-2A-1, 47G-3, 47G-3B, 47G-3B-1,
47G-3B-2, 47G-3B-2A, 47G-4, 47G-4A, 47G-5, 47G-5A, 47H-1, 47J, 47J-2, 47J-2A,
and 47K Helicopters | Main rotor blade box beam clip (clip)
| Bell Helicopter Textron | Bell Helicopter Textron,Bell Helicopter Textron,Bell Helicopter Textron,Bell Helicopter Textron,Bell Helicopter Textron,Bell Helicopter Textron,Bell Helicopter Textron,Bell Helicopter Textron,Bell Helicopter Textron,Bell Helicopter Textron,Bell Helicopter Textron,Bell Helicopter Textron,Bell Helicopter Textron,Bell Helicopter Textron,Bell Helicopter Textron,Bell Helicopter Textron,Bell Helicopter Textron,Bell Helicopter Textron,Bell Helicopter Textron,Bell Helicopter Textron,Bell Helicopter Textron,Bell Helicopter Textron,Bell Helicopter Textron | Bell Helicopter Textron 47B,Bell Helicopter Textron 47B3,Bell Helicopter Textron 47D,Bell Helicopter Textron 47D1,Bell Helicopter Textron 47E,Bell Helicopter Textron 47G,Bell Helicopter Textron 47G-2,Bell Helicopter Textron 47G-2A,Bell Helicopter Textron 47G-2A-1,Bell Helicopter Textron 47G-3,Bell Helicopter Textron 47G-3B,Bell Helicopter Textron 47G-3B-1,Bell Helicopter Textron 47G-3B-2,Bell Helicopter Textron 47G-3B-2A,Bell Helicopter Textron 47G-4,Bell Helicopter Textron 47G-4A,Bell Helicopter Textron 47G-5,Bell Helicopter Textron 47G-5A,Bell Helicopter Textron 47H-1,Bell Helicopter Textron 47J,Bell Helicopter Textron 47J-2,Bell Helicopter Textron 47J-2A,Bell Helicopter Textron 47K | 47B,47B3,47D,47D1,47E,47G,47G-2,47G-2A,47G-2A-1,47G-3,47G-3B,47G-3B-1,47G-3B-2,47G-3B-2A,47G-4,47G-4A,47G-5,47G-5A,47H-1,47J,47J-2,47J-2A,47K | Part 39 | Airworthiness Directives | 05/19/2009 | 1 | 2009-12-01.pdf | 88293 |
| 2009-11-13 | FAA-2009-0498 | 39-15923 | 06/17/2009 | 06/02/2009 | | | | Learjet Model 45 Airplanes | Hydraulic power | Learjet Inc. | Learjet Inc. | Learjet Inc. 45 | 45 | Part 39 | Airworthiness Directives | 05/20/2009 | 1 | 2009-11-13.pdf | 40410 |
| 2009-11-12 | FAA-2008-1201 | 39-15922 | 08/25/2009 | 07/21/2009 | 2004-14-06 | | | Airbus Model A310 Series Airplanes | Wing root | Airbus | Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus | Airbus A310-203,Airbus A310-204,Airbus A310-221,Airbus A310-222,Airbus A310-304,Airbus A310-322,Airbus A310-324,Airbus A310-325 | A310-203,A310-204,A310-221,A310-222,A310-304,A310-322,A310-324,A310-325 | Part 39 | Airworthiness Directives | 07/02/2009 | 1 | 2009-11-12.pdf | 37651 |
| 2009-11-11 | FAA-2009-0213 | 39-15921 | 07/07/2009 | 06/02/2009 | | | | McDonnell Douglas Model MD-90-30 Airplanes | Fuel | McDonnell Douglas Corporation | McDonnell Douglas Corporation | McDonnell Douglas Corporation MD-90-30 | MD-90-30 | Part 39 | Airworthiness Directives | 05/20/2009 | 1 | 2009-11-11.pdf | 28862 |
| 2009-11-10 | FAA-2009-0482 | 39-15920 | 06/12/2009 | 05/28/2009 | | | | Eurocopter Deutschland GmbH Model EC135 Helicopters | Main rotor drive | Eurocopter Deutschland GmbH | Eurocopter Deutschland GmbH | Eurocopter Deutschland GmbH EC135 | EC135 | Part 39 | Airworthiness Directives | 05/19/2009 | 1 | 2009-11-10.pdf | 34807 |
| 2009-11-09 | FAA-2009-0486 | 39-15919 | 06/12/2009 | 05/29/2009 | | | | Airbus Model A310 Airplanes and Airbus Model A300-600
Airplanes | Equipment/Furnishings
| Airbus | Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus | Airbus A300B4-601,Airbus A300B4-603,Airbus A300B4-605R,Airbus A300B4-620,Airbus A300B4-622R,Airbus A300F4-605R,Airbus A300F4-622R,Airbus A300^ Model B4-622,Airbus A300^ Model C4-605 Variant F,Airbus A310-203,Airbus A310-204,Airbus A310-221,Airbus A310-222,Airbus A310-304,Airbus A310-322,Airbus A310-324,Airbus A310-325 | A300B4-601,A300B4-603,A300B4-605R,A300B4-620,A300B4-622R,A300F4-605R,A300F4-622R,A300, Model B4-622,A300, Model C4-605 Variant F,A310-203,A310-204,A310-221,A310-222,A310-304,A310-322,A310-324,A310-325 | Part 39 | Airworthiness Directives | 05/15/2009 | 1 | 2009-11-09.pdf | 38404 |
| 2009-11-08 | FAA-2009-0479 | 39-15918 | 06/12/2009 | 05/28/2009 | | | | Airbus Model A330-202, -223, -243, - 301, -322, and
-342 Airplanes | Fuselage
| Airbus | Airbus,Airbus,Airbus,Airbus,Airbus,Airbus | Airbus A330-202,Airbus A330-223,Airbus A330-243,Airbus A330-301,Airbus A330-322,Airbus A330-342 | A330-202,A330-223,A330-243,A330-301,A330-322,A330-342 | Part 39 | Airworthiness Directives | 05/15/2009 | 1 | 2009-11-08.pdf | 36018 |
| 2009-11-07 | FAA-2009-0478 | 39-15917 | 06/12/2009 | 05/28/2009 | | | | British Aerospace Model HS 748 Airplanes | Fuel | BAE Systems (Operations) Limited | BAE Systems (Operations) Limited,BAE Systems (Operations) Limited | BAE Systems (Operations) Limited HS 748 Series 2A,BAE Systems (Operations) Limited HS 748 Series 2B | HS 748 Series 2A,HS 748 Series 2B | Part 39 | Airworthiness Directives | 05/15/2009 | 1 | 2009-11-07.pdf | 38586 |
| 2009-11-06 | FAA-2009-0119 | 39-15916 | 07/02/2009 | 05/28/2009 | 2008-12-16 | | | M7 Aerospace LP Models SA226-AT, SA226- T, SA226-TC,
SA227-AC (C-26A), SA227-AT, SA227-BC (C-26A), SA227-CC, and SA227-DC (C-26B)
Airplanes | Hydraulic tube assemblies
| M7 Aerospace LP | M7 Aerospace LP,M7 Aerospace LP,M7 Aerospace LP,M7 Aerospace LP,M7 Aerospace LP,M7 Aerospace LP,M7 Aerospace LP,M7 Aerospace LP | M7 Aerospace LP SA226-AT,M7 Aerospace LP SA226-T,M7 Aerospace LP SA226-TC,M7 Aerospace LP SA227-AC (C-26A),M7 Aerospace LP SA227-AT,M7 Aerospace LP SA227-BC (C-26A),M7 Aerospace LP SA227-CC,M7 Aerospace LP SA227-DC (C-26B) | SA226-AT,SA226-T,SA226-TC,SA227-AC (C-26A),SA227-AT,SA227-BC (C-26A),SA227-CC,SA227-DC (C-26B) | Part 39 | Airworthiness Directives | 05/18/2009 | 1 | 2009-11-06.pdf | 37976 |
| 2009-11-05 | FAA-2009-0473 | 39-15915 | 05/08/2008 | 05/22/2009 | 2008-10-12 | | | Air Tractor, Inc. Models AT-400, AT- 400A, AT-402,
AT-402A, AT-402B, AT-502, AT-502A, AT-502B, AT-503A, AT- 602, AT-802, and
AT-802A Airplanes | Cracks in the engine mount
| Air Tractor^ Inc. | Air Tractor, Inc.,Air Tractor, Inc.,Air Tractor, Inc.,Air Tractor, Inc.,Air Tractor, Inc.,Air Tractor, Inc.,Air Tractor, Inc.,Air Tractor, Inc.,Air Tractor, Inc.,Air Tractor, Inc.,Air Tractor, Inc.,Air Tractor, Inc. | Air Tractor^ Inc. AT-400,Air Tractor^ Inc. AT-400A,Air Tractor^ Inc. AT-402,Air Tractor^ Inc. AT-402A,Air Tractor^ Inc. AT-402B,Air Tractor^ Inc. AT-502,Air Tractor^ Inc. AT-502A,Air Tractor^ Inc. AT-502B,Air Tractor^ Inc. AT-503A,Air Tractor^ Inc. AT-602,Air Tractor^ Inc. AT-802,Air Tractor^ Inc. AT-802A | AT-400,AT-400A,AT-402,AT-402A,AT-402B,AT-502,AT-502A,AT-502B,AT-503A,AT-602,AT-802,AT-802A | Part 39 | Airworthiness Directives | 05/15/2009 | 1 | 2009-11-05_Corrected.pdf | 36357 |
| 2009-11-04 | FAA-2009-0082 | 39-15914 | 06/26/2009 | 06/11/2009 | | | | Rolls-Royce Corporation AE 2100D2, AE 2100D2A, AE
2100D3, and AE 2100J Turboprop Engines | Propeller gearbox (PGB) | Rolls-Royce Corporation | Rolls-Royce Corporation,Rolls-Royce Corporation,Rolls-Royce Corporation,Rolls-Royce Corporation | Rolls-Royce Corporation AE 2100D2,Rolls-Royce Corporation AE 2100D2A,Rolls-Royce Corporation AE 2100D3,Rolls-Royce Corporation AE 2100J | AE 2100D2,AE 2100D2A,AE 2100D3,AE 2100J | Part 39 | Airworthiness Directives | 05/14/2009 | 1 | 2009-11-04.pdf | 34677 |
| 2009-11-03 | FAA-2009-0462 | 39-15913 | 06/04/2009 | 05/20/2009 | | | | Lockheed Model 382, 382B, 382E, 382F, and 382G Series
Airplanes | Wings
| Lockheed Martin Corporation | Lockheed Martin Corporation,Lockheed Martin Corporation,Lockheed Martin Corporation,Lockheed Martin Corporation,Lockheed Martin Corporation | Lockheed Martin Corporation 382,Lockheed Martin Corporation 382B,Lockheed Martin Corporation 382E,Lockheed Martin Corporation 382F,Lockheed Martin Corporation 382G | 382,382B,382E,382F,382G | Part 39 | Airworthiness Directives | 05/07/2009 | 1 | 2009-11-03.pdf | 35094 |
| 2009-11-02 | FAA-2008-1245 | 39-15912 | 06/23/2009 | 05/19/2009 | | | | CFM International S.A. Model CFM56 Turbofan Engines | HPC 4-9 spools
| CFM International^ S.A. | CFM International, S.A.,CFM International, S.A.,CFM International, S.A.,CFM International, S.A.,CFM International, S.A.,CFM International, S.A.,CFM International, S.A.,CFM International, S.A.,CFM International, S.A.,CFM International, S.A.,CFM International, S.A.,CFM International, S.A.,CFM International, S.A.,CFM International, S.A.,CFM International, S.A.,CFM International, S.A.,CFM International, S.A.,CFM International, S.A.,CFM International, S.A.,CFM International, S.A.,CFM International, S.A.,CFM International, S.A.,CFM International, S.A.,CFM International, S.A.,CFM International, S.A.,CFM International, S.A.,CFM International, S.A.,CFM International, S.A.,CFM International, S.A.,CFM International, S.A.,CFM International, S.A.,CFM International, S.A.,CFM International, S.A.,CFM International, S.A.,CFM International, S.A.,CFM International, S.A.,CFM International, S.A.,CFM International, S.A.,CFM International, S.A.,CFM International, S.A.,CFM International, S.A.,CFM International, S.A.,CFM International, S.A.,CFM International, S.A.,CFM International, S.A.,CFM International, S.A.,CFM International, S.A.,CFM International, S.A.,CFM International, S.A.,CFM International, S.A.,CFM International, S.A.,CFM International, S.A.,CFM International, S.A.,CFM International, S.A.,CFM International, S.A.,CFM International, S.A.,CFM International, S.A.,CFM International, S.A.,CFM International, S.A.,CFM International, S.A.,CFM International, S.A.,CFM International, S.A.,CFM International, S.A.,CFM International, S.A.,CFM International, S.A.,CFM International, S.A.,CFM International, S.A.,CFM International, S.A.,CFM International, S.A.,CFM International, S.A.,CFM International, S.A.,CFM International, S.A.,CFM International, S.A.,CFM International, S.A.,CFM International, S.A.,CFM International, S.A.,CFM International, S.A.,CFM International, S.A.,CFM International, S.A.,CFM International, S.A.,CFM International, S.A.,CFM International, S.A.,CFM International, S.A.,CFM International, S.A.,CFM International, S.A.,CFM International, S.A.,CFM International, S.A.,CFM International, S.A.,CFM International, S.A.,CFM International, S.A.,CFM International, S.A.,CFM International, S.A.,CFM International, S.A.,CFM International, S.A.,CFM International, S.A.,CFM International, S.A. | CFM International^ S.A. CFM56-2,CFM International^ S.A. CFM56-2A,CFM International^ S.A. CFM56-2B,CFM International^ S.A. CFM56-3,CFM International^ S.A. CFM56-3B,CFM International^ S.A. CFM56-3C,CFM International^ S.A. CFM56-5,CFM International^ S.A. CFM56-5-A1/F,CFM International^ S.A. CFM56-5A4,CFM International^ S.A. CFM56-5A4/F,CFM International^ S.A. CFM56-5A5,CFM International^ S.A. CFM56-5A5/F,CFM International^ S.A. CFM56-5B1,CFM International^ S.A. CFM56-5B1/2P,CFM International^ S.A. CFM56-5B1/3,CFM International^ S.A. CFM56-5B1/P,CFM International^ S.A. CFM56-5B2,CFM International^ S.A. CFM56-5B2/2P,CFM International^ S.A. CFM56-5B2/3,CFM International^ S.A. CFM56-5B2/P,CFM International^ S.A. CFM56-5B3/2P,CFM International^ S.A. CFM56-5B3/3,CFM International^ S.A. CFM56-5B3/3B1,CFM International^ S.A. CFM56-5B3/P,CFM International^ S.A. CFM56-5B3/P1,CFM International^ S.A. CFM56-5B4,CFM International^ S.A. CFM56-5B4/2P,CFM International^ S.A. CFM56-5B4/2P1,CFM International^ S.A. CFM56-5B4/3,CFM International^ S.A. CFM56-5B4/3B1,CFM International^ S.A. CFM56-5B4/P,CFM International^ S.A. CFM56-5B4/P1,CFM International^ S.A. CFM56-5B5,CFM International^ S.A. CFM56-5B5/3,CFM International^ S.A. CFM56-5B5/P,CFM International^ S.A. CFM56-5B6,CFM International^ S.A. CFM56-5B6/2P,CFM International^ S.A. CFM56-5B6/3,CFM International^ S.A. CFM56-5B6/P,CFM International^ S.A. CFM56-5B7,CFM International^ S.A. CFM56-5B7/3,CFM International^ S.A. CFM56-5B7/P,CFM International^ S.A. CFM56-5B8/3,CFM International^ S.A. CFM56-5B8/P,CFM International^ S.A. CFM56-5B9/2P,CFM International^ S.A. CFM56-5B9/3,CFM International^ S.A. CFM56-5B9/P,CFM International^ S.A. CFM56-5C2,CFM International^ S.A. CFM56-5C2/4,CFM International^ S.A. CFM56-5C2/F,CFM International^ S.A. CFM56-5C2/F4,CFM International^ S.A. CFM56-5C2/G,CFM International^ S.A. CFM56-5C2/G4,CFM International^ S.A. CFM56-5C2/P,CFM International^ S.A. CFM56-5C3/F,CFM International^ S.A. CFM56-5C3/F4,CFM International^ S.A. CFM56-5C3/G,CFM International^ S.A. CFM56-5C3/G4,CFM International^ S.A. CFM56-5C3/P,CFM International^ S.A. CFM56-5C4,CFM International^ S.A. CFM56-5C4/1,CFM International^ S.A. CFM56-5C4/1P,CFM International^ S.A. CFM56-5C4/P,CFM International^ S.A. CFM56-7B20,CFM International^ S.A. CFM56-7B20/2,CFM International^ S.A. CFM56-7B20/3,CFM International^ S.A. CFM56-7B22,CFM International^ S.A. CFM56-7B22/2,CFM International^ S.A. CFM56-7B22/3,CFM International^ S.A. CFM56-7B22/3B1,CFM International^ S.A. CFM56-7B22/B1,CFM International^ S.A. CFM56-7B24,CFM International^ S.A. CFM56-7B24/2,CFM International^ S.A. CFM56-7B24/3,CFM International^ S.A. CFM56-7B24/3B1,CFM International^ S.A. CFM56-7B24/B1,CFM International^ S.A. CFM56-7B26,CFM International^ S.A. CFM56-7B26/2,CFM International^ S.A. CFM56-7B26/3,CFM International^ S.A. CFM56-7B26/3B1,CFM International^ S.A. CFM56-7B26/3B2,CFM International^ S.A. CFM56-7B26/3B2F,CFM International^ S.A. CFM56-7B26/3F,CFM International^ S.A. CFM56-7B26/B1,CFM International^ S.A. CFM56-7B26/B2,CFM International^ S.A. CFM56-7B27,CFM International^ S.A. CFM56-7B27A,CFM International^ S.A. CFM56-7B27A/3,CFM International^ S.A. CFM56-7B27/2,CFM International^ S.A. CFM56-7B27/3,CFM International^ S.A. CFM56-7B27/3B1,CFM International^ S.A. CFM56-7B27/3B1F,CFM International^ S.A. CFM56-7B27/3B3,CFM International^ S.A. CFM56-7B27/3F,CFM International^ S.A. CFM56-7B27/B1,CFM International^ S.A. CFM56-7B27/B3 | CFM56-2,CFM56-2A,CFM56-2B,CFM56-3,CFM56-3B,CFM56-3C,CFM56-5,CFM56-5-A1/F,CFM56-5A4,CFM56-5A4/F,CFM56-5A5,CFM56-5A5/F,CFM56-5B1,CFM56-5B1/2P,CFM56-5B1/3,CFM56-5B1/P,CFM56-5B2,CFM56-5B2/2P,CFM56-5B2/3,CFM56-5B2/P,CFM56-5B3/2P,CFM56-5B3/3,CFM56-5B3/3B1,CFM56-5B3/P,CFM56-5B3/P1,CFM56-5B4,CFM56-5B4/2P,CFM56-5B4/2P1,CFM56-5B4/3,CFM56-5B4/3B1,CFM56-5B4/P,CFM56-5B4/P1,CFM56-5B5,CFM56-5B5/3,CFM56-5B5/P,CFM56-5B6,CFM56-5B6/2P,CFM56-5B6/3,CFM56-5B6/P,CFM56-5B7,CFM56-5B7/3,CFM56-5B7/P,CFM56-5B8/3,CFM56-5B8/P,CFM56-5B9/2P,CFM56-5B9/3,CFM56-5B9/P,CFM56-5C2,CFM56-5C2/4,CFM56-5C2/F,CFM56-5C2/F4,CFM56-5C2/G,CFM56-5C2/G4,CFM56-5C2/P,CFM56-5C3/F,CFM56-5C3/F4,CFM56-5C3/G,CFM56-5C3/G4,CFM56-5C3/P,CFM56-5C4,CFM56-5C4/1,CFM56-5C4/1P,CFM56-5C4/P,CFM56-7B20,CFM56-7B20/2,CFM56-7B20/3,CFM56-7B22,CFM56-7B22/2,CFM56-7B22/3,CFM56-7B22/3B1,CFM56-7B22/B1,CFM56-7B24,CFM56-7B24/2,CFM56-7B24/3,CFM56-7B24/3B1,CFM56-7B24/B1,CFM56-7B26,CFM56-7B26/2,CFM56-7B26/3,CFM56-7B26/3B1,CFM56-7B26/3B2,CFM56-7B26/3B2F,CFM56-7B26/3F,CFM56-7B26/B1,CFM56-7B26/B2,CFM56-7B27,CFM56-7B27A,CFM56-7B27A/3,CFM56-7B27/2,CFM56-7B27/3,CFM56-7B27/3B1,CFM56-7B27/3B1F,CFM56-7B27/3B3,CFM56-7B27/3F,CFM56-7B27/B1,CFM56-7B27/B3 | Part 39 | Airworthiness Directives | 05/13/2009 | 1 | 2009-11-02.pdf | 31348 |
| 2009-11-01 | FAA-2009-0453 | 39-15911 | 06/12/2009 | 05/28/2009 | 95-21-12 | | | Eurocopter Deutschland GmbH (ECD) Model MBB-BK 117
A-1, A-3, A-4, B-1, B-2, and C-1 Helicopters | Main rotor blades | Eurocopter Deutschland GmbH | Eurocopter Deutschland GmbH,Eurocopter Deutschland GmbH,Eurocopter Deutschland GmbH,Eurocopter Deutschland GmbH,Eurocopter Deutschland GmbH,Eurocopter Deutschland GmbH | Eurocopter Deutschland GmbH MBB-BK 117 A-1,Eurocopter Deutschland GmbH MBB-BK 117 A-3,Eurocopter Deutschland GmbH MBB-BK 117 A-4,Eurocopter Deutschland GmbH MBB-BK 117 B-1,Eurocopter Deutschland GmbH MBB-BK 117 B-2,Eurocopter Deutschland GmbH MBB-BK 117 C-1 | MBB-BK 117 A-1,MBB-BK 117 A-3,MBB-BK 117 A-4,MBB-BK 117 B-1,MBB-BK 117 B-2,MBB-BK 117 C-1 | Part 39 | Airworthiness Directives | 05/07/2009 | 1 | 2009-11-01.pdf | 34074 |
| 2009-10-14 | FAA-2009-0114 | 39-15910 | 06/04/2009 | 05/20/2009 | | | | Hartzell Propeller Inc. Steel Hub Turbine Propellers | Steel hub turbine propellers | Hartzell Propeller^ Inc. | Hartzell Propeller, Inc.,Hartzell Propeller, Inc.,Hartzell Propeller, Inc.,Hartzell Propeller, Inc.,Hartzell Propeller, Inc.,Hartzell Propeller, Inc.,Hartzell Propeller, Inc.,Hartzell Propeller, Inc.,Hartzell Propeller, Inc.,Hartzell Propeller, Inc. | Hartzell Propeller^ Inc. HC-A3MV,Hartzell Propeller^ Inc. HC-A3V,Hartzell Propeller^ Inc. HC-B3T,Hartzell Propeller^ Inc. HC-B4MP-3,Hartzell Propeller^ Inc. HC-B4TN-5,Hartzell Propeller^ Inc. HC-B5MA-2,Hartzell Propeller^ Inc. HC-B5MA-3,Hartzell Propeller^ Inc. HC-B5MA-5,Hartzell Propeller^ Inc. HC-B5MP-3,Hartzell Propeller^ Inc. HC-B5MP-5 | HC-A3MV,HC-A3V,HC-B3T,HC-B4MP-3,HC-B4TN-5,HC-B5MA-2,HC-B5MA-3,HC-B5MA-5,HC-B5MP-3,HC-B5MP-5 | Part 39 | Airworthiness Directives | 05/08/2009 | 1 | 2009-10-14.pdf | 35370 |
| 2009-10-13 | FAA-2009-0035 | 39-15909 | 06/24/2009 | 05/20/2009 | | | | Saab AB, Saab Aerosystems Model 340A (SAAB/SF340A)
and SAAB 340B Airplanes | Powerplant
| Saab AB^ Saab Aerosystems | Saab AB, Saab Aerosystems,Saab AB, Saab Aerosystems | Saab AB^ Saab Aerosystems 340A (SAAB SF340A),Saab AB^ Saab Aerosystems SAAB 340B | 340A (SAAB SF340A),SAAB 340B | Part 39 | Airworthiness Directives | 05/06/2009 | 1 | 2009-10-13.pdf | 32061 |
| 2009-10-12 | FAA-2009-0450 | 39-15908 | 06/04/2009 | 05/20/2009 | 2005-16-06 | | | Boeing Model 747 Airplanes | Equipment/Furnishings | Boeing Company^ The | Boeing Company, The,Boeing Company, The,Boeing Company, The,Boeing Company, The,Boeing Company, The,Boeing Company, The,Boeing Company, The,Boeing Company, The,Boeing Company, The,Boeing Company, The,Boeing Company, The,Boeing Company, The | Boeing Company^ The 747-100 Series,Boeing Company^ The 747-100B Series,Boeing Company^ The 747-100B SUD Series,Boeing Company^ The 747-200B Series,Boeing Company^ The 747-200C Series,Boeing Company^ The 747-200F Series,Boeing Company^ The 747-300 Series,Boeing Company^ The 747-400 Series,Boeing Company^ The 747-400D Series,Boeing Company^ The 747-400F Series,Boeing Company^ The 747SP Series,Boeing Company^ The 747SR Series | 747-100 Series,747-100B Series,747-100B SUD Series,747-200B Series,747-200C Series,747-200F Series,747-300 Series,747-400 Series,747-400D Series,747-400F Series,747SP Series,747SR Series | Part 39 | Airworthiness Directives | 05/06/2009 | 1 | 2009-10-12.pdf | 40930 |
| 2009-10-11 | FAA-2009-0449 | 39-15907 | 06/04/2009 | 05/20/2009 | | | | Airbus Model A330-300, A340-200, and A340-300 Series
Airplanes | Stabilizers | Airbus | Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus | Airbus A330-301,Airbus A330-302,Airbus A330-303,Airbus A330-321,Airbus A330-322,Airbus A330-323,Airbus A330-341,Airbus A330-342,Airbus A330-343,Airbus A340-211,Airbus A340-212,Airbus A340-213,Airbus A340-311,Airbus A340-312,Airbus A340-313 | A330-301,A330-302,A330-303,A330-321,A330-322,A330-323,A330-341,A330-342,A330-343,A340-211,A340-212,A340-213,A340-311,A340-312,A340-313 | Part 39 | Airworthiness Directives | 05/06/2009 | 1 | 2009-10-11.pdf | 37823 |
| 2009-10-10 | FAA-2009-0448 | 39-15906 | 05/29/2009 | 05/14/2009 | | | | Bombardier Model CL-600-2C10 (Regional Jet Series
700, 701 & 702), CL-600-2D15 (Regional Jet Series 705), and CL-600-2D24
(Regional Jet Series 900) Airplanes | Air Conditioning | Bombardier Inc. | Bombardier Inc.,Bombardier Inc.,Bombardier Inc. | Bombardier Inc. CL-600-2C10 (Regional Jet Series 700),Bombardier Inc. CL-600-2C10 (Regional Jet Series 701),Bombardier Inc. CL-600-2C10 (Regional Jet Series 702) | CL-600-2C10 (Regional Jet Series 700),CL-600-2C10 (Regional Jet Series 701),CL-600-2C10 (Regional Jet Series 702) | Part 39 | Airworthiness Directives | 05/06/2009 | 1 | 2009-10-10.pdf | 38101 |
| 2009-10-09 R1 | FAA-2007-27747 | 39-16074 | 12/11/2009 | 11/06/2009 | 2009-10-09 | | | Cessna Aircraft Company 150 and 152 Series Airplanes | Rudder stop | Cessna Aircraft Company | Cessna Aircraft Company,Cessna Aircraft Company,Cessna Aircraft Company,Cessna Aircraft Company,Cessna Aircraft Company,Cessna Aircraft Company,Cessna Aircraft Company,Cessna Aircraft Company,Cessna Aircraft Company,Cessna Aircraft Company,Cessna Aircraft Company,Cessna Aircraft Company,Cessna Aircraft Company,Cessna Aircraft Company,Cessna Aircraft Company,Cessna Aircraft Company,Cessna Aircraft Company,Cessna Aircraft Company,Cessna Aircraft Company,Cessna Aircraft Company,Cessna Aircraft Company,Cessna Aircraft Company,Cessna Aircraft Company,Cessna Aircraft Company,Cessna Aircraft Company | Cessna Aircraft Company 150F,Cessna Aircraft Company 150G,Cessna Aircraft Company 150H,Cessna Aircraft Company 150J,Cessna Aircraft Company 150K,Cessna Aircraft Company 150L,Cessna Aircraft Company 150M,Cessna Aircraft Company 152,Cessna Aircraft Company A150K,Cessna Aircraft Company A150L,Cessna Aircraft Company A152,Cessna Aircraft Company F150F,Cessna Aircraft Company F150G,Cessna Aircraft Company F150H,Cessna Aircraft Company F150J,Cessna Aircraft Company F150K,Cessna Aircraft Company F150L,Cessna Aircraft Company F150M,Cessna Aircraft Company F152,Cessna Aircraft Company FA150K,Cessna Aircraft Company FA150L,Cessna Aircraft Company FA150M,Cessna Aircraft Company FA152,Cessna Aircraft Company FRA150L,Cessna Aircraft Company FRA150M | 150F,150G,150H,150J,150K,150L,150M,152,A150K,A150L,A152,F150F,F150G,F150H,F150J,F150K,F150L,F150M,F152,FA150K,FA150L,FA150M,FA152,FRA150L,FRA150M | Part 39 | Airworthiness Directives | 10/27/2009 | 1 | 2009-10-09 R1.pdf | 36478 |
| 2009-10-09 | FAA-2007-27747 | 39-15904 | 06/17/2009 | 05/13/2009 | | | | Cessna Aircraft Company 150 and 152 Series Airplanes | Rudder stop | Cessna Aircraft Company | Cessna Aircraft Company,Cessna Aircraft Company,Cessna Aircraft Company,Cessna Aircraft Company,Cessna Aircraft Company,Cessna Aircraft Company,Cessna Aircraft Company,Cessna Aircraft Company,Cessna Aircraft Company,Cessna Aircraft Company,Cessna Aircraft Company,Cessna Aircraft Company,Cessna Aircraft Company,Cessna Aircraft Company,Cessna Aircraft Company,Cessna Aircraft Company,Cessna Aircraft Company,Cessna Aircraft Company,Cessna Aircraft Company,Cessna Aircraft Company,Cessna Aircraft Company,Cessna Aircraft Company,Cessna Aircraft Company,Cessna Aircraft Company | Cessna Aircraft Company 150F,Cessna Aircraft Company 150G,Cessna Aircraft Company 150H,Cessna Aircraft Company 150J,Cessna Aircraft Company 150K,Cessna Aircraft Company 150L,Cessna Aircraft Company 150M,Cessna Aircraft Company 152,Cessna Aircraft Company A150K,Cessna Aircraft Company A150L,Cessna Aircraft Company A150M,Cessna Aircraft Company A152,Cessna Aircraft Company F150F,Cessna Aircraft Company F150G,Cessna Aircraft Company F150H,Cessna Aircraft Company F150J,Cessna Aircraft Company F150K,Cessna Aircraft Company F150L,Cessna Aircraft Company F150M,Cessna Aircraft Company F152,Cessna Aircraft Company FA150K,Cessna Aircraft Company FA150L,Cessna Aircraft Company FA150M,Cessna Aircraft Company FA152 | 150F,150G,150H,150J,150K,150L,150M,152,A150K,A150L,A150M,A152,F150F,F150G,F150H,F150J,F150K,F150L,F150M,F152,FA150K,FA150L,FA150M,FA152 | Part 39 | Airworthiness Directives | 05/05/2009 | 1 | 2009-10-09.pdf | 40846 |
| 2009-10-08 | FAA-2008-1131 | 39-15903 | 06/17/2009 | 05/13/2009 | | | | Pratt & Whitney Models PW2037, PW2037(M), and PW2040
Turbofan Engines | High-pressure turbine 2nd stage hubs that have previously been exposed to Pratt & Whitney cleaning procedure SPOP 10 or SPOP 9 or equivalent procedure. | Pratt & Whitney Division | Pratt & Whitney Division,Pratt & Whitney Division,Pratt & Whitney Division | Pratt & Whitney Division PW2037,Pratt & Whitney Division PW2037M,Pratt & Whitney Division PW2040 | PW2037,PW2037M,PW2040 | Part 39 | Airworthiness Directives | 05/04/2009 | 1 | 2009-10-08.pdf | 38236 |
| 2009-10-07 | FAA-2009-0433 | 39-15902 | 05/28/2009 | 05/13/2009 | | | | Airbus Model A380-841, -842, and -861 Airplanes | Air Transport Association (ATA) of America Code 57: Wings.
| Airbus | Airbus,Airbus,Airbus | Airbus A380-841,Airbus A380-842,Airbus A380-861 | A380-841,A380-842,A380-861 | Part 39 | Airworthiness Directives | 05/01/2009 | 1 | 2009-10-07.pdf | 34924 |
| 2009-10-06 | FAA-2009-0135 | 39-15901 | 06/17/2009 | 05/13/2009 | | | | Boeing Model 747-400 and 747-400D Series Airplanes | Air Transport Association (ATA) of America Code 27: Flight controls. | Boeing Company^ The | Boeing Company, The,Boeing Company, The | Boeing Company^ The 747-400 Series,Boeing Company^ The 747-400D Series | 747-400 Series,747-400D Series | Part 39 | Airworthiness Directives | 05/01/2009 | 1 | 2009-10-06.pdf | 29470 |
| 2009-10-05 | FAA-2009-0428 | 39-15900 | 05/28/2009 | 05/13/2009 | | | | Bombardier Model CL-600-2B19 (Regional Jet Series 100
and 440) Airplanes | Air Transport Association (ATA) of America Code 27: Flight controls.
| Bombardier Inc. | Bombardier Inc.,Bombardier Inc. | Bombardier Inc. CL-600-2B19 (Regional Jet Series 100),Bombardier Inc. CL-600-2B19 (Regional Jet Series 440) | CL-600-2B19 (Regional Jet Series 100),CL-600-2B19 (Regional Jet Series 440) | Part 39 | Airworthiness Directives | 04/30/2009 | 1 | 2009-10-05.pdf | 36966 |
| 2009-10-04 | FAA-2009-0240 | 39-15899 | 06/17/2009 | 05/13/2009 | 2007-17-06 | | | Diamond Aircraft Industries GmbH Model DA 40 and DA
40 F Airplanes | Air Transport Association of America (ATA) Code 32: Landing gear.
| Diamond Aircraft Industries GmbH | Diamond Aircraft Industries GmbH,Diamond Aircraft Industries GmbH | Diamond Aircraft Industries GmbH DA 40,Diamond Aircraft Industries GmbH DA 40F | DA 40,DA 40F | Part 39 | Airworthiness Directives | 05/01/2009 | 1 | 2009-10-04.pdf | 34976 |
| 2009-10-03 | FAA-2009-0419 | 39-15898 | 05/26/2009 | 05/08/2009 | | | | 328 Support Services GmbH Dornier Model 328-100 and
-300 Airplanes | Flight controls
| 328 Support Services GmbH | 328 Support Services GmbH,328 Support Services GmbH | 328 Support Services GmbH 328-100,328 Support Services GmbH 328-300 | 328-100,328-300 | Part 39 | Airworthiness Directives | 04/29/2009 | 1 | 2009-10-03.pdf | 32242 |
| 2009-10-02 | FAA-2008-1214 | 39-15897 | 06/11/2009 | 05/07/2009 | 2005-19-15 | | | BAE Systems (Operations) Limited (Jetstream) Model
4101 Airplanes | Main landing gear (MLG) | BAE Systems (Operations) Limited | BAE Systems (Operations) Limited | BAE Systems (Operations) Limited Jetstream Model 4101 | Jetstream Model 4101 | Part 39 | Airworthiness Directives | 04/27/2009 | 1 | 2009-10-02.pdf | 30954 |
| 2009-10-01 | FAA-2006-23742 | 39-15896 | 06/09/2009 | 05/18/2009 | | | | Correction: Pratt & Whitney (PW) JT9D-7R4 Series Turbofan Engines | High-pressure turbine (HPT) vane assemblies | Pratt & Whitney Division | Pratt & Whitney Division,Pratt & Whitney Division,Pratt & Whitney Division,Pratt & Whitney Division | Pratt & Whitney Division JT9D-7R4E1,Pratt & Whitney Division JT9D-7R4E4,Pratt & Whitney Division JT9D-7R4G2,Pratt & Whitney Division JT9D-7R4H1 | JT9D-7R4E1,JT9D-7R4E4,JT9D-7R4G2,JT9D-7R4H1 | Part 39 | Correction | 04/23/2009 | 1 | 2009-10-01_Correction.pdf | 30225 |
| 2009-09-51 | Unknown | | | | | | | Emergency AD: Eurocopter France Model EC225LP helicopters | Main gearbox | Eurocopter France | Eurocopter France | Eurocopter France EC225LP | EC225LP | Part 39 | Emergency AD | 04/17/2009 | 1 | 2009-09-51_Emergency.pdf | 30295 |
| 2009-09-09 | FAA-2009-0395 | 39-15895 | 05/11/2009 | 04/30/2009 | | | | Cessna Aircraft Company (Type Certificate Previously
Held by Columbia Aircraft Manufacturing (Previously The Lancair Company))
Models LC40-550FG, LC41-550FG, and LC42-550FG Airplanes | Rudder hinge brackets | Cessna Aircraft Company | Cessna Aircraft Company,Cessna Aircraft Company,Cessna Aircraft Company | Cessna Aircraft Company LC40-550FG,Cessna Aircraft Company LC41-550FG,Cessna Aircraft Company LC42-550FG | LC40-550FG,LC41-550FG,LC42-550FG | Part 39 | Airworthiness Directives | 04/23/2009 | 1 | 2009-09-09.pdf | 32597 |
| 2009-09-08 | FAA-2008-1239 | 39-15894 | 06/11/2009 | 05/07/2009 | | | | Boeing Model 747 Airplanes | Upper lobe doubler
| Boeing Company^ The | Boeing Company, The,Boeing Company, The,Boeing Company, The,Boeing Company, The,Boeing Company, The,Boeing Company, The,Boeing Company, The,Boeing Company, The,Boeing Company, The,Boeing Company, The,Boeing Company, The,Boeing Company, The | Boeing Company^ The 747-100 Series,Boeing Company^ The 747-100B Series,Boeing Company^ The 747-100B SUD Series,Boeing Company^ The 747-200B Series,Boeing Company^ The 747-200C Series,Boeing Company^ The 747-200F Series,Boeing Company^ The 747-300 Series,Boeing Company^ The 747-400 Series,Boeing Company^ The 747-400D Series,Boeing Company^ The 747-400F Series,Boeing Company^ The 747SP Series,Boeing Company^ The 747SR Series | 747-100 Series,747-100B Series,747-100B SUD Series,747-200B Series,747-200C Series,747-200F Series,747-300 Series,747-400 Series,747-400D Series,747-400F Series,747SP Series,747SR Series | Part 39 | Airworthiness Directives | 04/22/2009 | 1 | 2009-09-08.pdf | 29968 |
| 2009-09-07 | FAA-2008-1070 | 39-15893 | 06/11/2009 | 05/07/2009 | | | | Boeing Model 737-100, -200, -200C, - 300, -400, and
-500 Series Airplanes | Retract actuator beam | Boeing Company^ The | Boeing Company, The,Boeing Company, The,Boeing Company, The,Boeing Company, The,Boeing Company, The,Boeing Company, The | Boeing Company^ The 737-100 Series,Boeing Company^ The 737-200 Series,Boeing Company^ The 737-200C Series,Boeing Company^ The 737-300 Series,Boeing Company^ The 737-400 Series,Boeing Company^ The 737-500 Series | 737-100 Series,737-200 Series,737-200C Series,737-300 Series,737-400 Series,737-500 Series | Part 39 | Airworthiness Directives | 04/22/2009 | 1 | 2009-09-07.pdf | 29583 |
| 2009-09-06 | FAA-2008-1275 | 39-15892 | 06/11/2009 | 05/07/2009 | | | | Boeing Model 737-100, -200, -200C, - 300, -400, and
-500 Series Airplanes | Backup intercostals | Boeing Company^ The | Boeing Company, The,Boeing Company, The,Boeing Company, The,Boeing Company, The,Boeing Company, The,Boeing Company, The | Boeing Company^ The 737-100 Series,Boeing Company^ The 737-200 Series,Boeing Company^ The 737-200C Series,Boeing Company^ The 737-300 Series,Boeing Company^ The 737-400 Series,Boeing Company^ The 737-500 Series | 737-100 Series,737-200 Series,737-200C Series,737-300 Series,737-400 Series,737-500 Series | Part 39 | Airworthiness Directives | 04/22/2009 | 1 | 2009-09-06.pdf | 27464 |
| 2009-09-05 | FAA-2007-0391 | 39-15891 | 06/04/2009 | 04/30/2009 | 2006-03-10 | | | Airbus Model A318-100 and A319-100 Series Airplanes;
A320-111 Airplanes; A320-200 Series Airplanes; and A321-100 and A321-200 Series
Airplanes | Horizontal hinge pin | Airbus | Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus | Airbus A318 Model -111,Airbus A318 Model -112,Airbus A319 Model -111,Airbus A319 Model -112,Airbus A319 Model -113,Airbus A319 Model -114,Airbus A319 Model -115,Airbus A319 Model -131,Airbus A319 Model -132,Airbus A319 Model -133,Airbus A320 Model -111,Airbus A320 Model -211,Airbus A320 Model -212,Airbus A320 Model -214,Airbus A320 Model -231,Airbus A320 Model -232,Airbus A320 Model -233,Airbus A321 Model-212,Airbus A321 Model-213,Airbus A321 Model-232,Airbus A321 Model -111,Airbus A321 Model -112,Airbus A321 Model -131,Airbus A321 Model -211,Airbus A321 Model -231 | A318 Model -111,A318 Model -112,A319 Model -111,A319 Model -112,A319 Model -113,A319 Model -114,A319 Model -115,A319 Model -131,A319 Model -132,A319 Model -133,A320 Model -111,A320 Model -211,A320 Model -212,A320 Model -214,A320 Model -231,A320 Model -232,A320 Model -233,A321 Model-212,A321 Model-213,A321 Model-232,A321 Model -111,A321 Model -112,A321 Model -131,A321 Model -211,A321 Model -231 | Part 39 | Airworthiness Directives | 04/15/2009 | 1 | 2009-09-05.pdf | 27079 |
| 2009-09-04 | FAA-2009-0371 | 39-15890 | 05/18/2009 | 04/27/2009 | | 2009-14-10 | | EADS-PZL "Warszawa-Okecie'' S.A. Model PZL-104 WILGA
80 Airplanes | Fuselage
| EADS-PZL Warszawa-Okecie S.A. | EADS-PZL Warszawa-Okecie S.A. | EADS-PZL Warszawa-Okecie S.A. PZL-104 WILGA 80 | PZL-104 WILGA 80 | Part 39 | Airworthiness Directives | 04/15/2009 | 1 | 2009-09-04.pdf | 141701 |
| 2009-09-03 | FAA-2007-28077 | 39-15889 | 06/01/2009 | 04/27/2009 | | | | Turbomeca S.A. Arriel 2B and 2B1 Turboshaft Engines | Turbine blade
| Turbomeca S.A. | Turbomeca S.A.,Turbomeca S.A. | Turbomeca S.A. Arriel 2B,Turbomeca S.A. Arriel 2B1 | Arriel 2B,Arriel 2B1 | Part 39 | Airworthiness Directives | 04/16/2009 | 1 | 2009-09-03.pdf | 26161 |
| 2009-09-02 | FAA-2009-0361 | 39-15888 | 05/06/2009 | 04/21/2009 | | | | Bombardier Model DHC-8-400 Series Airplanes | Landing gear
| Bombardier Inc. | Bombardier Inc. | Bombardier Inc. DHC-8-400 Series | DHC-8-400 Series | Part 39 | Airworthiness Directives | 04/08/2009 | 1 | 2009-09-02.pdf | 36413 |
| 2009-09-01 | FAA-2009-0360 | 39-15887 | 05/06/2009 | 04/21/2009 | | | | Airbus Model A318, A319, A320 and A321 Series
Airplanes | Wings
| Airbus | Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus,Airbus | Airbus A318 Model -111,Airbus A318 Model -112,Airbus A318 Model -121,Airbus A318 Model -122,Airbus A319 Model -111,Airbus A319 Model -112,Airbus A319 Model -113,Airbus A319 Model -114,Airbus A319 Model -115,Airbus A319 Model -131,Airbus A319 Model -132,Airbus A319 Model -133,Airbus A320 Model -111,Airbus A320 Model -211,Airbus A320 Model -212,Airbus A320 Model -214,Airbus A320 Model -231,Airbus A320 Model -232,Airbus A320 Model -233,Airbus A321 Model-212,Airbus A321 Model-213,Airbus A321 Model-232,Airbus A321 Model -111,Airbus A321 Model -112,Airbus A321 Model -131,Airbus A321 Model -211,Airbus A321 Model -231 | A318 Model -111,A318 Model -112,A318 Model -121,A318 Model -122,A319 Model -111,A319 Model -112,A319 Model -113,A319 Model -114,A319 Model -115,A319 Model -131,A319 Model -132,A319 Model -133,A320 Model -111,A320 Model -211,A320 Model -212,A320 Model -214,A320 Model -231,A320 Model -232,A320 Model -233,A321 Model-212,A321 Model-213,A321 Model-232,A321 Model -111,A321 Model -112,A321 Model -131,A321 Model -211,A321 Model -231 | Part 39 | Airworthiness Directives | 04/08/2009 | 1 | 2009-09-01.pdf | 34027 |
| 2009-08-51 | Unknown | | | | 2008-26-06 | | | Emergency AD: Rolls-Royce Corporation (RRC) AE 3007A series turbofan engines | High-pressure turbine stage 2 wheels | | Rolls-Royce Corporation (Indiana) | Rolls-Royce Corporation AE 3007A | AE 3007A | Part 39 | Emergency AD | 04/10/2009 | 1 | 2009-08-51_Emergency.pdf | 22140 |
| 2009-08-11 | FAA-2009-0126 | 39-15884 | 05/26/2009 | 04/21/2009 | | | | PILATUS AIRCRAFT LTD. Models PC-12 and PC-12/45
Airplanes | Ice and Rain Protection
| Pilatus Aircraft Limited | Pilatus Aircraft Limited,Pilatus Aircraft Limited | Pilatus Aircraft Limited PC-12,Pilatus Aircraft Limited PC-12/45 | PC-12,PC-12/45 | Part 39 | Airworthiness Directives | 04/09/2009 | 1 | 2009-08-11.pdf | 27616 |
| 2009-08-10 | FAA-2009-0347 | 39-15883 | 04/20/2009 | 04/15/2009 | 2009-04-14 | | | Pilatus Aircraft Ltd. Model PC-12/47E Airplanes | Primary Flight Displays (PFDs)
| Pilatus Aircraft Limited | Pilatus Aircraft Limited | Pilatus Aircraft Limited PC-12/47E | PC-12/47E | Part 39 | Airworthiness Directives | 04/08/2009 | 1 | 2009-08-10.pdf | 31432 |
| 2009-08-09 | FAA-2009-0124 | 39-15882 | 05/20/2009 | 04/15/2009 | | | | EADS SOCATA Model TBM 700 Airplanes | Wiring harness | SOCATA | SOCATA | SOCATA TBM 700 | TBM 700 | Part 39 | Airworthiness Directives | 04/03/2009 | 1 | 2009-08-09.pdf | 28234 |
| 2009-08-08 | FAA-2009-0302 | 39-15881 | 04/29/2009 | 04/14/2009 | | | | Turbomeca Arriel 1B, 1D, 1D1, 2B, and 2B1 Turboshaft
Engines | Power turbine blades
| Turbomeca S.A. | Turbomeca S.A.,Turbomeca S.A.,Turbomeca S.A. | Turbomeca S.A. Arriel 1B,Turbomeca S.A. Arriel 1D,Turbomeca S.A. Arriel 1D1 | Arriel 1B,Arriel 1D,Arriel 1D1 | Part 39 | Airworthiness Directives | 04/06/2009 | 1 | 2009-08-08.pdf | 30188 |
| 2009-08-07 | FAA-2008-1207 | 39-15880 | 05/18/2009 | 04/13/2009 | | | | Honeywell International Inc. ALF502L-2 and ALF502L-2C
Turbofan Engines | High-pressure compressor (HPC) first stage discs | Honeywell International Inc. | Honeywell International Inc.,Honeywell International Inc. | Honeywell International Inc. ALF502L-2,Honeywell International Inc. ALF502L-2C | ALF502L-2,ALF502L-2C | Part 39 | Airworthiness Directives | 04/06/2009 | 1 | 2009-08-07.pdf | 173907 |
| 2009-08-06 | FAA-2008-0827 | 39-15879 | 05/18/2009 | 04/13/2009 | | | | General Electric Company (GE) CF6-80A Series Turbofan
Engines | Stage 1 high-pressure turbine (HPT) rotor
disks | General Electric Company | General Electric Aircraft Engines,General Electric Aircraft Engines,General Electric Aircraft Engines,General Electric Aircraft Engines | General Electric Company CF6-80A,General Electric Company CF6-80A1,General Electric Company CF6-80A2,General Electric Company CF6-80A3 | CF6-80A,CF6-80A1,CF6-80A2,CF6-80A3 | Part 39 | Airworthiness Directives | 04/06/2009 | 1 | 2009-08-06.pdf | 24167 |
| 2009-08-05 | FAA-2009-0329 | 39-15878 | 04/20/2009 | 04/09/2009 | | | | Liberty Aerospace Incorporated Model XL-2 Airplanes | Exhaust muffler | Liberty Aerospace Incorporated | Liberty Aerospace Incorporated | Liberty Aerospace Incorporated XL-2 | XL-2 | Part 39 | Airworthiness Directives | 04/03/2009 | 1 | 2009-08-05.pdf | 34375 |
| 2009-08-04 | FAA-2008-1240 | 39-15877 | 05/14/2009 | 04/09/2009 | | | | Hawker Beechcraft Corporation Model BH.125 Series
600A Airplanes and Model HS.125 Series 700A Airplanes Modified in Accordance
With Supplemental Type Certificate (STC) SA2271SW | Wiring diagrams
| Hawker Beechcraft Corporation | Hawker Beechcraft Corporation,Hawker Beechcraft Corporation | Hawker Beechcraft Corporation BH.125 Series 600A,Hawker Beechcraft Corporation HS.125 Series 700A | BH.125 Series 600A,HS.125 Series 700A | Part 39 | Airworthiness Directives | 04/02/2009 | 1 | 2009-08-04.pdf | 25261 |
| 2009-08-03 | FAA-2009-0301 | 39-15876 | 04/24/2009 | 04/09/2009 | 2007-19-52
2007-19-52 | | | Bell Helicopter Textron Canada Limited Model 206A,
206B, 206L, 206L-1, 206L-3, 206L-4, 222, 222B, 222U, 230, 407, 427, and 430
Helicopters | Tail rotor blade (blade) | Bell Helicopter Textron (Canada) | Bell Helicopter Textron (Canada),Bell Helicopter Textron (Canada),Bell Helicopter Textron (Canada),Bell Helicopter Textron (Canada),Bell Helicopter Textron (Canada),Bell Helicopter Textron (Canada),Bell Helicopter Textron (Canada),Bell Helicopter Textron (Canada),Bell Helicopter Textron (Canada),Bell Helicopter Textron (Canada),Bell Helicopter Textron (Canada),Bell Helicopter Textron (Canada),Bell Helicopter Textron (Canada) | Bell Helicopter Textron (Canada) 206A,Bell Helicopter Textron (Canada) 206B,Bell Helicopter Textron (Canada) 206L,Bell Helicopter Textron (Canada) 206L-1,Bell Helicopter Textron (Canada) 206L-3,Bell Helicopter Textron (Canada) 206L-4,Bell Helicopter Textron (Canada) 222,Bell Helicopter Textron (Canada) 222B,Bell Helicopter Textron (Canada) 222U,Bell Helicopter Textron (Canada) 230,Bell Helicopter Textron (Canada) 407,Bell Helicopter Textron (Canada) 427,Bell Helicopter Textron (Canada) 430 | 206A,206B,206L,206L-1,206L-3,206L-4,222,222B,222U,230,407,427,430 | Part 39 | Airworthiness Directives | 03/26/2009 | 1 | 2009-08-03.pdf | 32093 |
| 2009-08-02 | FAA-2008-1324 | 39-15875 | 05/13/2009 | 04/08/2009 | | | | McDonnell Douglas Model DC-8-50 Series Airplanes;
Model DC-8F-54 and DC-8F-55 Airplanes; Model DC-8-60 Series Airplanes; Model
DC-8-60F Series Airplanes; Model DC-8-70 Series Airplanes; and Model DC-8-70F
Series Airplanes | Fuel pumps | McDonnell Douglas Corporation | McDonnell Douglas Corporation,McDonnell Douglas Corporation,McDonnell Douglas Corporation,McDonnell Douglas Corporation,McDonnell Douglas Corporation,McDonnell Douglas Corporation,McDonnell Douglas Corporation,McDonnell Douglas Corporation,McDonnell Douglas Corporation,McDonnell Douglas Corporation,McDonnell Douglas Corporation,McDonnell Douglas Corporation,McDonnell Douglas Corporation,McDonnell Douglas Corporation,McDonnell Douglas Corporation,McDonnell Douglas Corporation,McDonnell Douglas Corporation,McDonnell Douglas Corporation | McDonnell Douglas Corporation DC-8-51,McDonnell Douglas Corporation DC-8-52,McDonnell Douglas Corporation DC-8-53,McDonnell Douglas Corporation DC-8-55,McDonnell Douglas Corporation DC-8-61,McDonnell Douglas Corporation DC-8-61F,McDonnell Douglas Corporation DC-8-62,McDonnell Douglas Corporation DC-8-62F,McDonnell Douglas Corporation DC-8-63,McDonnell Douglas Corporation DC-8-63F,McDonnell Douglas Corporation DC-8-71,McDonnell Douglas Corporation DC-8-71F,McDonnell Douglas Corporation DC-8-72,McDonnell Douglas Corporation DC-8-72F,McDonnell Douglas Corporation DC-8-73,McDonnell Douglas Corporation DC-8-73F,McDonnell Douglas Corporation DC-8F-54,McDonnell Douglas Corporation DC-8F-55 | DC-8-51,DC-8-52,DC-8-53,DC-8-55,DC-8-61,DC-8-61F,DC-8-62,DC-8-62F,DC-8-63,DC-8-63F,DC-8-71,DC-8-71F,DC-8-72,DC-8-72F,DC-8-73,DC-8-73F,DC-8F-54,DC-8F-55 | Part 39 | Airworthiness Directives | 03/30/2009 | 1 | 2009-08-02.pdf | 23335 |
| 2009-08-01 | FAA-2008-0899 | 39-15874 | 05/14/2009 | 04/09/2009 | 2007-07-12 | | | Honeywell Flight Management Systems (FMSs) Equipped
With Honeywell NZ-2000 Navigation Computers and Honeywell IC-800 or IC-800E
Integrated Avionics Computers; as Installed on Various Transport Category
Airplanes | Honeywell FMSs | Bombardier Inc.,Dassault Aviation,Gulfstream Aerospace Corporation,Hawker Beechcraft Corporation,Lockheed Martin Corporation | Bombardier Inc.,Bombardier Inc.,Bombardier Inc.,Dassault Aviation,Gulfstream Aerospace Corporation,Gulfstream Aerospace Corporation,Gulfstream Aerospace Corporation,Gulfstream Aerospace Corporation,Hawker Beechcraft Corporation,Hawker Beechcraft Corporation,Hawker Beechcraft Corporation,Hawker Beechcraft Corporation,Hawker Beechcraft Corporation,Lockheed Martin Corporation | Bombardier Inc. CL-600-2B16 (CL-601-3A),Bombardier Inc. CL-600-2B16 (CL-601-3R),Bombardier Inc. CL-600-2B16 (CL-604),Dassault Aviation Mystere-Falcon 900,Gulfstream Aerospace Corporation G-1159A,Gulfstream Aerospace Corporation G-IV,Gulfstream Aerospace Corporation GV,Gulfstream Aerospace Corporation GV-SP,Hawker Beechcraft Corporation BAe.125 Series 800A,Hawker Beechcraft Corporation BAe.125 Series 800A (C-29A),Hawker Beechcraft Corporation BAe.125 Series 800A (U-125),Hawker Beechcraft Corporation Hawker 1000,Hawker Beechcraft Corporation Hawker 800XP,Lockheed Martin Corporation 382G | CL-600-2B16 (CL-601-3A),CL-600-2B16 (CL-601-3R),CL-600-2B16 (CL-604),Mystere-Falcon 900,G-1159A,G-IV,GV,GV-SP,BAe.125 Series 800A,BAe.125 Series 800A (C-29A),BAe.125 Series 800A (U-125),Hawker 1000,Hawker 800XP,382G | Part 39 | Airworthiness Directives | 03/30/2009 | 1 | 2009-08-01.pdf | 33418 |
| 2009-07-53 | Unknown | | | | | 2009-13-01 | | Emergency AD: Sikorsky Aircraft Corporation | Main gearbox filter bowl assembly | Sikorsky Aircraft Corporation | Sikorsky Aircraft Corporation | Sikorsky Aircraft Corporation S-92A | S-92A | Part 39 | Emergency AD | 03/23/2009 | 1 | 2009-07-53_Emergency.pdf | 23566 |
| 2009-07-52 | Unknown | | | | 2009-07-51 | | | Emergency AD: Bell Model 206A series, 206B series, 206L series, 407, and 427 helicopters | Lever assembly | Bell Helicopter Textron (Canada) | Bell Helicopter Textron (Canada),Bell Helicopter Textron (Canada),Bell Helicopter Textron (Canada),Bell Helicopter Textron (Canada),Bell Helicopter Textron (Canada),Bell Helicopter Textron (Canada),Bell Helicopter Textron (Canada),Bell Helicopter Textron (Canada),Bell Helicopter Textron (Canada),Bell Helicopter Textron (Canada) | Bell Helicopter Textron (Canada) 206A,Bell Helicopter Textron (Canada) 206A-1 (OH-58A),Bell Helicopter Textron (Canada) 206B,Bell Helicopter Textron (Canada) 206B-1,Bell Helicopter Textron (Canada) 206L,Bell Helicopter Textron (Canada) 206L-1,Bell Helicopter Textron (Canada) 206L-3,Bell Helicopter Textron (Canada) 206L-4,Bell Helicopter Textron (Canada) 407,Bell Helicopter Textron (Canada) 427 | 206A,206A-1 (OH-58A),206B,206B-1,206L,206L-1,206L-3,206L-4,407,427 | Part 39 | Emergency AD | 03/19/2009 | 1 | 2009-07-52_Emergency.pdf | 19382 |
|