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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 601 - 620 of 5103 | View All
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AD No. MAKE Condensed description of ad note
08-14-3 Bell Determine if the correct number and type of washers are installed, the tailboom bolt is oriented in the correct direction and then correct number of bolt threads are exposed in accordance with the notes in the AD | 206A, 206B, 206L, L1, L3, L4
08-14-13 Cirrus If threaded sleeve is or is not installed at the cabin door rod end install the appropriate rod end kit | SR20, SR22
08-14-1 Bell Rewire the No. 1 and No. 2 engines' fuel valve switch as specified | 222, 222B, 222U, 230, 430
08-13-6 Cessna Inspect the left and right wing electrical wire bundles at the anchor attach points for loose and damaged wiring | 208, 208B
08-13-51 Eclipse Superseded by 08-16-15
08-13-4 Dassault Determine whether any wing anti-ice flexible hose having P/N FAL1006 or ARM224A is installed and replace as sepcified | Falcon 20
08-13-31 Dassault Modify the existing engine cowls' locking system as specified if applicable | Falcon 2000
08-13-30 Gulfstream Inspect/replace fastner bolts used to attach the scissors to the horizontal and vertical stabilizers and update AFM as specified | Astra SPX, 1125 Westwind, G100
08-13-28 Hartzell Propeller Perform an initial ECI of the area around the lubrication holes of the hub blade sockets | Piper Seneca, Seminole, Beech 76
08-13-27 Turbomeca Replace the engine module 02 with a module that incorporates Turbomeca modification TF 12A as specified | Arrius 2F
08-13-17 Beechcraft Replace all affected circuit breaker toggle switches on applicable models as specified | Various Bonanzas and Barons
08-13-16 Pratt & Whitney Inspect low pressure compressor fan blades and replace as specified | PW305A, 305B
08-13-15 Embraer Superseded by 11-1-1
08-13-11 DeHavilland Develop a schedule for doing the initial and repeat CTs required in the AD | DHC-6-200, -300
08-13-10 Dassault Revise the Limitations Section of the AFM to include the AD information | Falcon 7X
08-12-7 Embraer Remove the sealant used to protect the LH and RH clear ice wiring conduits at the holes through the wing spars and install Teflon spiral as specified | Legacy
08-12-19 Dassault Inspect for damage of the feeder cable bundle at the right side partition wall at frame 22/23 and repair as specified | Falcon 900, 900EX
08-12-18 Dassault Check the integrity of the GP bus and IRS2 and repair them as applicable | 2000EX, 900EX
08-12-15 Dassault Replace the passenger oxygen mask boxes as specified | Falcon 900EX and 2000EX
08-12-14 Dassault Modify the electrical wiring of the wings' anti-ice system as specified | Falcon 2000EX

Showing Results 601 - 620 of 5103 | View All
< Previous | 26 | 27 | 28 | 29 | 30 | 31 | 32 | 33 | 34 | 35 | Next >

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