| 11-27-9 |
Socata |
Unsafe condition as installation of the wrong (switched) aileron control cables in the wing | TBM 700 |
| 11-27-6 |
Dassault Falcon |
AD prompted by a report of incorrect design of the transformer rectifier unit part of the ram air turbine system | Falcon 7X |
| 11-27-4 |
Beechcraft |
AD applies to applicable aircraft equipped with (STC) SA1762SO | 95-C55, D55, E55, 58, 58A |
| 11-27-1 |
Turbomeca |
AD to prevent over-temp damage of the GG turbine, which could result in an uncommanded in-flight shutdown | Arriel 1B |
| 11-26-7 |
TCM engines and Rolls Royce |
Supersedes 02-13-4 | Replace magneto as specified | Inspect removed magneto as directed | C125,C145,O300,IO-360,TSIO360,LTISO520AE |
| 11-26-4 |
Lycoming |
Supersedes 08-14-7 | Inspect/replace fuel injector fuel lines | select engines |
| 11-26-10 |
Enstrom |
AD defines an unsafe condition as a failure in the cyclic trim condition | F-28C,C-2,F; 280C,F,FX; Th-28,480,480B |
| 11-26-1 |
Piaggio |
AD to detect and correct baggage door lockpins that do not engage properly and modify as specified | P-180 |
| 11-25-51 |
Continental Motors |
Superseded by 12-10-13 |
| 11-25-4 |
Quest Aircraft |
Inspect the torque of the IPS bolt as specified | Kodiak 100 |
| 11-25-3 |
Bombardier |
AD issued to prevent fatigue cracking of the main landing gear prior to the published life limitation | 45 |
| 11-25-12 |
Pratt & Whitney |
Inspect the chip detector on the propeller reduction gearbox assembly for metal debris as specified | PT6A-15AG,-27,-28,-34,-34AG,-34B,-36 |
| 11-24-7 |
Turbomeca |
Perform a one-time functional test of the engine to confirm proper engine operation | Arriel 2B |
| 11-24-2 |
Gulfstream |
AD issued to prevent penetration of the third fire extinguisher bottle by fragments released due to a failure of the APU rotor system | GV, GVSP |
| 11-24-11 |
Honeywell |
If applicable remove from service HPC2 discs | ALF502L-2C |
| 11-24-1 |
Piaggio |
Check for associated main landing gear actuator serial numbers for AD | P180 |
| 11-23-7 |
Gulfstream |
One-time inspection of the aileron control servo actuators as specified | G150, 200 |
| 11-23-3 |
Socata |
AD requires installation of a protection of the electrical wire at the standby compass connector | TBM 700 |
| 11-23-2 |
Bell |
Supersedes 10-3-3 | To detect an edge void, corrosion, or a crack on a M/R blade, see AD | 205B, 212 |
| 11-22-6 |
Eurocopter |
Superseded by 11-22-5 |
