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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 381 - 400 of 5103
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| AD No. |
MAKE |
Condensed description of ad note |
| 10-15-10 |
Piper |
Inspect the pilot and copilot control wheel columns for correct control wheel shaft installation | Multiple Piper models |
| 10-14-5 |
Bombardier |
Inspect and replace if required, system accumulators 1, 2, 3 and brake accumulators 2 and 3 | 600, 601, 604, 605 series |
| 10-14-21 |
Thielert Aircraft Engines |
Remove the blow-by oil separators listed in AD table as specified | DA-40, STCd PA-28-161, STCd Cessna 172 |
| 10-14-20 |
McCauley Propeller |
Applies to model 4HFR34C653/L106FA, see AD for details. |
| 10-14-2 |
Bombardier |
Inspect ADG part number and accomplish AD if applicable as specified | Challenger 604 |
| 10-13-8 |
Air Tractor |
Superseded by 10-17-18 |
| 10-13-7 |
Piper |
Replace V-band exhast couplings as specified | PA-32R-301T and PA-46-350P |
| 10-13-10 |
Ontic Engineering |
AD applies to propeller governors found on the following models 7GCAA, A36, DA40, check for applicability |
| 10-13-1 |
Microturbo |
See AD regarding APU turbine wheel | Eurocopter AS332 |
| 10-12-2 |
Turbomeca |
Replace any CS Board, P/N 0177997160 with a S/N from 241El to 1192EL (inclusive) as specified | Makila 1A and 1A1 |
| 10-12-1 |
Eurocopter |
Concerns cracks discovered in the area of the center cross-member at station X 2325 at the attachment point of the yaw channel ball-type control sheath stop | AS350B,BA,B1,B2,B3,D AS355E,F,F1,F2,N |
| 10-11-9 |
Thielert Engines |
If P/N applicable replace the existing PPRV as specified | TAE 125-01 and TAE 125-02-99 |
| 10-11-52 |
Sikorsky |
Inspect the nameplate for the No. 1 and No. 2 AHRS units to determine if P/N 145130-711, Mod status 18 is installed and then proceed as specified | S-76A, B, C |
| 10-11-51 |
Eurocopter |
Visually inspect the affected TGB control lever for cracking and remove or replace as specified if required | AS350B, BA, B1, B2, C, D, D1 and AS355E, F, F1, F2, N |
| 10-11-4 |
Teledyne Continental |
Supersedes 09-24-52 | Check for affected hydraulic lifters in regards to excessive wear | 240, 360, 420, 520, 550 series |
| 10-11-2 |
Gulfstream |
Supersedes 07-3-5 | Amend the AFM to include additional procedure for verifying complete closure and locking of the main entry door | Astra 1125, SPX, G100 |
| 10-11-15 |
Socata |
Inspect the fire extinguisher(s) installed or carried on board the airplane as specified | TBM 700 |
| 10-11-11 |
Learjet |
Revise Tire-Servicing Section of Learjet 60 MM as specified | Lear 60 |
| 10-11-10 |
Turbomeca |
Inspect third stage turbine wheel and remove any damaged wheels | Astazou XIV B and XIV H |
| 10-11-1 |
Embraer |
Revise the ALS of the Instructions for Continued Airworthiness to incorporate structural inspection item (SSI) 53-12-19's applicable tasks as specified | EMB-135BJ |
Showing Results 381 - 400 of 5103
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