// FAA AIRWORTHINESS DIRECTIVES
FAA Airworthiness Directives
Search AD numbers, titles, or models across the FAA database.
| No | AD Number | Title | Model | Superseded AD | Superseded By | Actions |
|---|---|---|---|---|---|---|
| 1 | FAA 2003-23-04 | Number 3 left and right emergency exit doors | 757-200 Series | FAA 91-01-05 | ||
| 2 | FAA 2003-07-13 | Torque tube couplings | 757-200 Series | 757-200CB Series | 757-200PF Series | FAA 92-25-01 | ||
| 3 | FAA 2002-19-03 | Crankshaft | IO-540-A1A5 | IO-540-AA1A5 | IO-540-AA1B5 | IO-540-AB1A5 | IO-540-AC1A5 | IO-540-AE1A5 | IO-540-B1A5 | IO-540-B1B5 | IO-540-B1C5 | IO-540-C1B5 | IO-540-C1C5 | IO-540-C2C | IO-540-C4B5 | IO-540-C4B5D | IO-540-C4C5 | IO-540-C4D5 | IO-540-C4D5D | IO-540-D4A5 | IO-540-D4B5 | IO-540-D4C5 | IO-540-E1A5 | IO-540-E1B5 | IO-540-E1C5 | IO-540-G1A5 | IO-540-G1B5 | IO-540-G1C5 | IO-540-G1D5 | IO-540-G1E5 | IO-540-G1F5 | IO-540-J4A5 | IO-540-K1A5 | IO-540-K1A5D | IO-540-K1B5 | IO-540-K1B5D | IO-540-K1C5 | IO-540-K1D5 | IO-540-K1E5 | IO-540-K1E5D | IO-540-K1F5 | IO-540-K1F5D | IO-540-K1G5 | IO-540-K1G5D | IO-540-K1H5 | IO-540-K1J5 | IO-540-K1J5D | IO-540-K1K5 | IO-540-K2A5 | IO-540-L1A5 | IO-540-L1A5D | IO-540-L1B5D | IO-540-L1C5 | IO-540-M1A5 | IO-540-M1A5D | IO-540-M1B5D | IO-540-M1C5 | IO-540-M2A5D | IO-540-N1A5 | IO-540-P1A5 | IO-540-R1A5 | IO-540-S1A5 | IO-540-T4A5D | IO-540-T4B5 | IO-540-T4B5D | IO-540-T4C5D | IO-540-U1A5D | IO-540-U1B5D | IO-540-V4A5 | IO-540-V4A5D | IO-540-W1A5 | IO-540-W1A5D | IO-540-W3A5D | LTIO-540-F2BD | LTIO-540-J2B | LTIO-540-J2BD | TIO-540-A2B | TIO-540-A2C | TIO-540-AE2A | TIO-540-AH1A | TIO-540-F2BD | TIO-540-J2B | TIO-540-J2BD | TIO-540-S1AD | TIO-540-U2A | TIO-540-W2A | FAA 2002-17-53 | ||
| 4 | FAA 2002-01-15 | Lubrication Passage and Link Assembly Joint in the Inboard and Outboard Flaps of Trailing Edge | 767-200 Series | 767-300 Series | 767-300F Series | FAA 2006-10-08 | ||
| 5 | FAA 2001-14-23 | Elevator Control Cable and Green System Hydraulic Pump | ATR72-101 | ATR72-102 | ATR72-201 | ATR72-202 | ATR72-211 | ATR72-212 | ATR72-212A | |||
| 6 | FAA 2001-01-12 | Fittings Connecting the Fuselage to Stiffener Rods | CN-235 | CN-235-100 | CN-235-200 | |||
| 7 | FAA 2000-14-16 | Tail Rotor System | 407 | FAA 99-06-15 | ||
| 8 | FAA 2000-02-25 | Airframe Pneumatic Deicing Boots | MU-2B-10 | MU-2B-15 | MU-2B-20 | MU-2B-25 | MU-2B-26 | MU-2B-26A | MU-2B-30 | MU-2B-35 | MU-2B-36 | MU-2B-36A | MU-2B-40 | MU-2B-60 | FAA 2010-10-17 | ||
| 9 | FAA 99-19-37 | Uplock Actuator | DHC-8-101 | DHC-8-102 | DHC-8-103 | DHC-8-106 | DHC-8-301 | DHC-8-311 | DHC-8-315 | |||
| 10 | FAA 99-04-08 | Main Landing Gear Hydraulic Actuators | 1900 | 1900C | 1900C (C-12J) | 1900D |