// 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| No | AD Number | Title | Model | Superseded AD | Superseded By | Actions |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 2008-22-18 | Ballistic Recovery Systems, Inc. (BRS) | 150 | 150A | 150B | 150C | 150D | 150E | 150F | 150G | 150H | 150J | 150K | 150L | 150M | 152 | A150K | A150L | A150M | A152 | |||
| 2 | FAA 2008-06-52 | High-pressure fuel line | TAE 125-02-99 | |||
| 3 | FAA 2007-18-09 | Braking and steering control units (BSCUs) | A318-111 | A318-112 | A318-121 | A318-122 | A319-111 | A319-112 | A319-113 | A319-114 | A319-115 | A319-131 | A319-132 | A319-133 | A320-111 | A320-211 | A320-212 | A320-214 | A320-231 | A320-232 | A320-233 | A321-212 | A321-213 | A321-232 | A321-111 | A321-112 | A321-131 | A321-211 | A321-231 | FAA 2005-24-06 | FAA 2013-25-07 | |
| 4 | FAA 2007-04-07 | V-band clamps | DHC-8-400 | DHC-8-401 | DHC-8-402 | |||
| 5 | FAA 2006-14-08 | Flight idle blade angles | MU-2B-26A | MU-2B-36A | MU-2B-40 | MU-2B-60 | |||
| 6 | FAA 2005-26-05 | Laminated shims | DHC-8-400 | DHC-8-401 | DHC-8-402 | |||
| 7 | FAA 2005-13-30 | Fuselage skin panels | 737-100 Series | 737-200 Series | 737-200C Series | FAA 2017-02-02 | ||
| 8 | FAA 2004-26-10 | Ice-impact Panels Installed in the Low Pressure (LP) Compressor Case | TAY 611-8 | TAY 620-15 | TAY 650-15 | TAY 651-54 | FAA 2004-05-22 | FAA 2007-26-19 | |
| 9 | FAA 2004-13-03 | First Stage Turbine Rotor Blades | Viper Mk. 601-22 | FAA 2005-07-10 | ||
| 10 | FAA 2003-25-10 | Center accessory compartment (CAC) | MD-11 | MD-11F | FAA 2000-24-12 |