|
|
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 521 - 540 of 5103
| View All
< Previous |
22
|
23
|
24
|
25
|
26
|
27
|
28
|
29
|
30
|
31
| Next >
| AD No. |
MAKE |
Condensed description of ad note |
| 08-6-16 |
Pacific Aerospace |
Inspect/correct the main wiring loom on the right hand side of the aircraft adjacent to the frames at station 114.34 and 119.84 to insure there are two pieces of protective sleeving installed as specified | 750XL |
| 08-5-9 |
Cessna |
Remove, modify, and reinstall crew seats as specified | 172R, S, 182T, T181T, 206H, T206H |
| 08-5-8 |
Dassault |
Verify life rafts are stowed correctly, with deployment straps outboard, in accordance with the instructions and specifications in Dassault SBs F50-480 and 480-1 | Falcon 50 |
| 08-5-7 |
Dassault |
Verify the correct assembly of the elevator bellcrank P/N listed and determine if installed properly, if found in reverse condition re-install as specified | Falcon 200, 20 series |
| 08-5-2 |
Embraer |
Supersedes 05-25-4 | Inspect skin, attachment fittings and control rods of rudder as specified | Legacy |
| 08-5-17 |
MD Helicopter |
Supersedes 06-8-12 | Replace tailboom attachments and assemblies as specified | 600N |
| 08-5-14 |
Navion |
Inspect the entire fuel system as specified | Navion,A,B,D,E,F,G,H |
| 08-5-11 |
Bellanca |
Supersedes 76-23-3 | Inspect exhaust system each 100 hrs | 17-30,-30A,-31,-31A |
| 08-4-9 |
Taylorcraft |
Supersedes 07-16-14 | Visually inspect left/right wing front struts for corrosion or cracking as specified | F19, 21, and 22 series |
| 08-4-5 |
Eurocopter |
Inspect the wiring harnesses for chafing and wear in the areas shown in Figure 1 of the Eurocopter Alert Service Bulletin EC135-53A-017, replace as specified | EC135 |
| 08-4-3 |
Eurocopter |
Inspect the tightening torque of the MRH to main rotor mast assembly attachment bolts as specified | AS-365N2, N3, C, C1, C2, N, N1 |
| 08-4-14 |
Dassault |
Supersedes 00-12-15 | Inspect and test emergency exit for discrepancies as specified | 2000, 900, 50, 200, 10 |
| 08-3-3 |
Embraer |
Inspect the components and lower skin of the elevators and observe movements of the control surfaces, comply with AD as applicable | EMB-135BJ |
| 08-3-2 |
Cessna |
Superseded by 12-2-2 |
| 08-3-16 |
Cirrus |
Inspect the rudder, aileron, and rudder-aileron interconnect rigging; correct any out-of-rig condition; and replace the attaching hardware for the rudder-aileron interconnect arm as specified | SR20 & SR22 |
| 08-3-15 |
Socata |
Supersedes 07-4-8 | Inspect pilot door locking stop-fittings for correct length, replace if incorrect | TBM 700 |
| 08-3-14 |
Piaggio |
Replace the emergency exit door pan assembly as specified | P-180 |
| 08-3-10 |
Cessna |
Inspect the lower wing skin structure, forward wing spars, lower fuselage skin, fairings, and external fairing frames for corrosion and proceed as specified | 525, -A, -B |
| 08-3-1 |
deHavilland |
Supersedes 83-2-2 | Modify & replace wing structure | DH-6-200, -300 |
| 08-26-6 |
Rolls Royce |
Remove engines for ECI of the HPT stage 2 wheels if applicable as specified | AE3007A series |
Showing Results 521 - 540 of 5103
| View All
< Previous |
22
|
23
|
24
|
25
|
26
|
27
|
28
|
29
|
30
|
31
| Next >
|
