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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 201 - 220 of 5103 | View All
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AD No. MAKE Condensed description of ad note
11-9-18 Dassault Install dedicated fuses on WOW proximity sensors as specified if applicable | Falcon 7X
11-8-6 Honeywell AD is due to reports of fatigue cracks in the airfoil of the power turbine blade, see AD for details | LTS-101-600A-2, -650B-1, -650C-2, -650C-3, -750C-1
11-8-1 Bell Helicopter Superseded by 13-3-16
11-7-13 CPAC Superseded by 12-2-10
11-7-11 Dassault Visually inspect the extinguishing system line and the low pressure bleed line of the number 2 engine at frame 42 in the rear compartment as specified | Falcon 50
11-7-10 Bombardier Supersedes 10-10-18 | Revise Airworthiness Limitations section of the Instructions for Continued Airworthiness as specified | Challenger 300
11-6-7 Eurocopter Helicopters with an applicable flotation gear unit, see AD for details | EC130B4
11-6-6 Eclipse Supersedes 08-24-7 | Applicable to EA500s with P&W610F-A engines; add text in AD to the Limitation's section of the AFM as specified | EA500
11-6-10 Piper Supersedes 99-15-4 | Perform turbine inlet temperature guage and probe cleaning, inspection and calibration and copy AD to POH | PA-46-350P
11-5-8 Turbomeca Supersedes 11-5-51 | AD propmted due to incorrectly assembled low-pressure fuel system ejectors, see for details | Arriel 1E2, 1S, 1S1
11-5-7 Allied Ag Cat Supersedes 08-22-21 | Inspect rudder tubular spar for corrosion | G164, A, G164B
11-5-51 Turbomeca Superseded by 11-5-8
11-5-1 Piaggio AD due to compass mismatch due to ferro-magnetic masses stowed in the baggage compartment, see for details | P-180
11-4-8 Bombardier Visually inspect for damage of wiring and correct routing in left & right circuit breaker panels as specified | Learjet 45
11-3-6 Eurocopter Remove and replace the aluminum T/R blade pitch control shaft with a steel shaft as specified | AS-365N2, N3 and SA-365N1
11-3-4 Cessna Supersedes 09-9-9 | Inspect/repair rudder hinges and hinge brackets as specified | LC-40, -41, -42
11-3-3 Bell Helicopter Inspect the tail rotor driveshaft hanger bearing bracket p/n 427-044-223-101 for cracks as specified | 427
11-3-2 Eurocopter Within the next 10 hours TIS do a functional test of the pedal unit adjustment system as specified | SA330J
11-3-16 Cessna AD to detect and correct overvoltage condition on the DC electrical busses caused by exciter stator winding failures | Citation X
11-3-12 Hawker Beechcraft Perform a detailed inspection for appropriate coverage of firewall sealant, left and right pylon firewall structure as specified | 400A and T

Showing Results 201 - 220 of 5103 | View All
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