| 10-26-51 |
Bell |
Supersedes 09-8-3 | Remove and replace each affected tail rotor blade as specified | 206 & 222 series, 230, 427, 430 |
| 10-26-5 |
Dassault |
Inspect for overpressure tightness on both regulating valves using an approved method | Falcon series |
| 10-26-4 |
Piper |
Applies to PA-28-161 equipped with Thielert Aircraft TAE-125-01, install backup battery system as specified | PA-28-161 |
| 10-26-3 |
Beechcraft |
Supersedes 08-7-10 | Replace tail deice boot pneumatic supply tubes and placard the airplane with the prohibition from flight in known or forecast icing as specified | B200, B200GT, B300, B300C |
| 10-25-51 |
Bell Helicopter |
Superseded by 11-8-1 |
| 10-25-5 |
Rolls-Royce |
AD issued to prevent failure of the HPT stage 1 and stage 2 discs, see AD for compliance | BR700-710A1-10 / -710A2-20 / -710C4-11 |
| 10-25-1 |
Diamond |
AD to change the emergency open doors procedure and retrofit the rear passenger door retaining bracket | DA40 and 40F |
| 10-24-8 |
Dassault |
Superseded by 11-10-14 |
| 10-24-52 |
Bell Helicopter |
Superseded by 10-25-51 |
| 10-24-51 |
Bell Helicopter |
Superseded by 10-24-52 |
| 10-24-5 |
Pratt & Whitney |
AD to prevent failure of the impeller, see for details | PW305A and B models |
| 10-24-3 |
Robinson |
Visually inspect each A359-1 (left) and A359-2 (right) pedal support for a crack as specified | R22 & R44 models |
| 10-24-2 |
Dassault |
Install a shield plate on the rear fuel tank structure as specified | Falcon 7X |
| 10-23-9 |
Austro Engine |
Superseded by 11-18-19 |
| 10-23-8 |
Bombardier |
Relates to balance washer screw failure on similar RATs/air driven generators, see AD for details | BD700-1A10 / -1A11 |
| 10-23-28 |
Socata |
Supersedes 09-23-12 | Revises AD 09-13-5, see AD for details | TBM700 |
| 10-23-23 |
Eurocopter |
Inspect the position of each upper and lower door catch and replace if necessary | SA330F,G,J / AS332C,L,L1,L2 |
| 10-23-2 |
Eurocopter |
Revise VNE airspeed operating limitation to 150 KIAS and rate of descent to not exceed 1,500 ft/min as specified | SA365N,N1; AS365N2,AS365N3 |
| 10-23-17 |
Diamond |
Inspect crankcase for cracks and replace if found as specified | DA-20 w/rotax |
| 10-23-16 |
Embraer |
Replace both flow control shutoff valves as specified | Phenom 100 |
