| 00-8-13 |
Lear |
Revise AFM to include TFM procedure for brake malfunction during taxi, take-off abort | 45 |
| 00-7-3 |
Robinson |
Inspect for chafing between wire harness and fuel line assembly | R44 |
| 00-7-25 |
Gulfstream |
Replace as specified alternator power feeder cables; install bracket, clamp or spacer and reroute | G-IV |
| 00-7-11 |
Piaggio |
This AD has Been rescinded | Inspect as specified brake system assembly for wear or damage | P-180 |
| 00-6-9 |
Turbomeca Engine |
Install module TU63 as specified | Eurocopter AS 355,N |
| 00-6-7 |
Eurocopter |
Record service history for main transmission tail rotor bevel gear TIS as specified; replace as directed | BK 117 |
| 00-6-6 |
New Piper |
Revise AFM Limitation Section on operation of deicing boots | Various models |
| 00-6-4 |
Fairchild |
Revise AFM Limitations Section on operation of deice boots as specified | SA 226 AT |
| 00-6-3 |
Bombardier |
Revise AFM on operation of deicing boots as specified | DHC-6 |
| 00-6-12 |
Turbomeca Engine |
Superseded by 02-22-11 |
| 00-6-11 |
Turbomeca Engine |
Inspect scavenge and lubrication system for coke deposit obstruction, repair as required; replace oil as specified | Eurocopter AS 332,330 |
| 00-6-10 |
Bell |
Superseded by 03-5-3 |
| 00-6-1 |
Cessna |
Measure stand pipe in fuel strainer assembly for specified length | 150, 152, 172, 182, 185, 188 |
| 00-5-6 |
Raytheon |
Inspect left and right engine fire extinguisher bottle squibs for incorrect wiring; re-label wiring | 400A |
| 00-5-24 |
Honeywell |
Inspect auto pilot server actuator for loose fastner | Various Cessna, Mooney and Piper models |
| 00-5-23 |
Ayres |
Replace main landing gear fuselage attach bolts as specified | S-2, 2R |
| 00-5-20 |
Dassault |
Inspect passenger oxygen masks for proper function | Falcon 900, 200, 50, 20 |
| 00-5-17 |
Eurocopter |
Inspect coupling tubes and engine mount fitting components for cracks, replace as specified.| EC 120B |
| 00-5-15 |
Eurocopter |
Superseded by 02-22-16 |
| 00-5-14 |
Allied Signal Engines |
Supersedes 80-22-53 | Rework oil inlet tube, turbine nozzle and fire shield | CL-600 |
