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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 141 - 160 of 5103 | View All
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AD No. MAKE Condensed description of ad note
12-21-51 Eurocopter Superseded by 12-25-4
12-21-5 Beechcraft Incorrect guage wiring | G58
12-21-11 Bombardier Oxygen cylinder | Challenger 601-3A, 3R
12-20-2 Eurocopter Non-conforming air filter elements | SA-365N1, AS-365N2, AS-365N3
12-2-6 Honeywell AD to prevent uncontained failure of the first stage turbine disk | TPE-331-10
12-2-51 Bell Reduced life limit of 3,600hr TIS to 1,400hr TIS as specified | 206L, L1, L3, L4
12-2-2 Cessna Supersedes 08-3-2 | Inspect the fuel return line assembly for chafing and proceed as specified | 172R & S
12-2-18 Dassault Prompted by reports of cracking of the flap tracks | Falcon 50
12-2-13 Eurocopter AD defines the unsafe condition as cracks on the tailboom/Fenestron | EC130B4
12-2-10 CPAC Supersedes 11-7-13 | Inspection of elevator spars to detect cracks | Commander 112,B,TC,TCA; 114,A,B,TC
12-19-1 Lycoming Crankshaft failure prevention | Various models
12-18-9 Bell Unsafe condition as an incorrect torque value of the tailboom attachment bolt | Bell 407
12-18-8 Eurocopter Unsafe condition from jammin of one of the fuel shut-off control levers | SA330F,G,J, AS332C,L,L1,L2
12-18-6 Piaggio Unsafe condition on an aviation product | P180
12-18-4 Tecnam Replace the landing gear emergency accumulator as specified | P2006T
12-18-18 Turbomeca AD to prevent rupture of a gas generator turbine blade | Arriel 2B1, 2B1, 2S2, 2C2
12-18-16 Cessna Replace aux power unit GCU | Citation X
12-18-1 M7 Aerospace Fatigue cracking in the left and right forward and aft spar wing-to-fuselage attach fittings | SA226 and SA227 series
12-17-9 Eurocopter Reduced service life of the rotating star | SA341G
12-17-8 Bell Crack in a yoke | 212

Showing Results 141 - 160 of 5103 | View All
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