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 181 - 200 of 4715
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| AD No. | MAKE | Condensed description of ad note |
|---|---|---|
| 08-8-6 | Bombardier | Superseded by 08-21-9 |
| 08-8-3 | Pacific Aerospace | Replace certain pitot heat sensor circuit breakers and add a cooling fan circuit as specified | 750XL |
| 08-7-11 | Pilatus | Insert updated documents into the airworthiness limitations section of the AFM as sepcified | PC-12,/45,/47 |
| 08-7-10 | Beechcraft | Replace the 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 |
| 08-7-8 | Pacific Aerospace | Inspect/replace to ensure that 1/8-inch rivets are not installed in place of the correct 5/32-inch rivets that secure the horizontal tail surface load transfer angles to the rearmost fuselage frame as specified | 750XL |
| 08-7-1 | Turbomeca | Supersedes 06-2-8 | Inspect 2nd stage turbine blades as specified | Arriel 1B |
| 08-6-51 | Continental/Lycoming | Superseded by 08-8-14 |
| 08-6-28 | Avidyne Corp | Perform a logbook inspection to determine if any PFD serial numbers are affected by this AD and then proceed as specified | Various Aircraft |
| 08-6-19 | Honeywell | Using the compliance schedule in the AD, remove and replace the LPC aft shaft as specified | ATF3-6-4C, AT3-6A-3C, -4C |
| 08-6-17 | Pilatus | Superseded by 09-5-7 |
| 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 |
| 08-5-17 | 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 |
| 08-5-9 | 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 |
| 08-4-14 | Dassault | Supersedes 00-12-15 | Inspect and test emergency exit for discrepancies as specified | 2000, 900, 50, 200, 10 |
| 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 |
Showing Results 181 - 200 of 4715
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