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.
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| AD No. | MAKE | Condensed description of ad note |
|---|---|---|
| 11-9-9 | Bombardier | Revisions to certain operator maintenance documents to include new inspections, see AD | Challenger 601,-3A,-3R; 604; 605 |
| 11-9-8 | Pacific Aerospace | Inspect the left and right-hand rudder pedal assemblies for cracks and incorporating a modification repair scheme if any cracks are found | 750XL |
| 11-9-51 | Piaggio | Supersedes 11-1-53 | Remove central floor panels in the cabin, inspect fuselage belly and functionally test the fuselage drain holes as specified | P180 |
| 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 | Supersedes 10-25-51 | Replace affected main rotor inboard strap fitting if applicable before further flight as specified | 212 |
| 11-7-13 | CPAC | Inspection of elevator spars to detect cracks | Commander 112,B,TC,TCA, 114,A,B,TC |
| 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 |
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