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Airworthiness Directives

NOTE - This AD note listing is intended as a guide only and should not be relied upon as conclusive evidence of AD applicability on any particular aircraft. Entire Airworthiness Directives may be accessed at: http://rgl.faa.gov.

Showing Results 221 - 240 of 5103 | View All
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AD No. MAKE Condensed description of ad note
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11-25-51 Continental Motors Superseded by 12-10-13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

Showing Results 221 - 240 of 5103 | View All
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