2026-18-05
final ruleAirworthiness Directives; Dassault Aviation Airplanes
Unsafe Condition: unsafe condition on these products.
Why matched: Airworthiness Directives; Dassault Aviation Airplanes
Search FAA Documents
274 results found (322ms)
2026-18-06
final ruleAirworthiness Directives; Gulfstream Aerospace LP (Type Certificate Previously Held by Israel Aircraft Industries, Ltd.) Airplanes
Unsafe Condition: unsafe condition on these products.
Why matched: Airworthiness Directives; Gulfstream Aerospace LP (Type Certificate Previously Held by Israel Aircraft Industries, Ltd.) Airplanes
2026-18-04 Recurring
final ruleAirworthiness Directives; Rolls-Royce Deutschland Ltd & Co KG Engines
Unsafe Condition: unsafe condition on these products.
Why matched: Airworthiness Directives; Rolls-Royce Deutschland Ltd & Co KG Engines
2026-18-02
final ruleAirworthiness Directives; Dassault Aviation Airplanes
Unsafe Condition: unsafe condition on these products.
Why matched: Airworthiness Directives; Dassault Aviation Airplanes
2026-17-08
final ruleAirworthiness Directives; Pratt & Whitney Division Engines
Unsafe Condition: Incorrect shot peening on high-pressure compressor (HPC) drum rotor disk assemblies.
Why matched: Airworthiness Directives; Pratt & Whitney Division Engines
2026-15-12
final ruleAirworthiness Directives; Pilatus Aircraft Ltd. Airplanes
Unsafe Condition: The emergency exit door could not be opened from inside the airplane.
Why matched: Airworthiness Directives; Pilatus Aircraft Ltd. Airplanes
2026-17-05
final ruleAirworthiness Directives; Various Helicopters
Unsafe Condition: Rescue hoist assemblies may have non-conformant overload clutch assemblies.
Why matched: Airworthiness Directives; Various Helicopters
2026-17-07
final ruleAirworthiness Directives; Leonardo S.p.A. Helicopters
Unsafe Condition: The incorrect installation of the swashplate duplex bearing could lead to bearing failure and subsequent loss of main rotor control.
Why matched: Airworthiness Directives; Leonardo S.p.A. Helicopters
2026-17-06
final ruleAirworthiness Directives; Rolls-Royce Deutschland Ltd & Co KG Engines
Unsafe Condition: Premature failure of certain lubrication/scavenge pumps causing engine in-flight shut-downs (IFSDs).
Why matched: Airworthiness Directives; Rolls-Royce Deutschland Ltd & Co KG Engines
2026-17-01
final ruleAirworthiness Directives; Airbus SAS Airplanes
Unsafe Condition: Cracks in the forward and aft upper corner of the bulk cargo door due to fatigue.
Why matched: Airworthiness Directives; Airbus SAS Airplanes
2026-17-02 Recurring
final ruleAirworthiness Directives; The Boeing Company Airplanes
Unsafe Condition: Shim gaps exceeding engineering allowances and high pull up forces on components may cause fatigue cracks at fastener holes in lower side of body splice plates, rear spar terminal fittings, lower c...
Why matched: Airworthiness Directives; The Boeing Company Airplanes
2026-17-04 Recurring
final ruleAirworthiness Directives; Airbus SAS Airplanes
Unsafe Condition: Failure of the main landing gear (MLG) door actuators could result in loss of MLG door function.
Why matched: Airworthiness Directives; Airbus SAS Airplanes
2026-17-03
final ruleAirworthiness Directives; International Aero Engines AG Engines
Unsafe Condition: Certain 3rd stage high pressure compressor (HPC) rotor blades were susceptible to shroud wear and blade failure.
Why matched: Airworthiness Directives; International Aero Engines AG Engines
2026-16-07
final ruleAirworthiness Directives; ATR-GIE Avions de Transport Régional Airplanes
Unsafe Condition: unsafe condition on these products.
Why matched: Airworthiness Directives; ATR-GIE Avions de Transport Régional Airplanes
2026-16-10 Recurring
final ruleAirworthiness Directives; Airbus Helicopters
Unsafe Condition: The unsafe condition involves excessive vibration levels on the tail rotor drive shaft, which could lead to failure of the tail rotor drive shaft, sliding flange, or equipped splined sleeve.
Why matched: Airworthiness Directives; Airbus Helicopters
2026-16-09
final ruleAirworthiness Directives; Gulfstream Aerospace LP (Type Certificate Previously Held by Israel Aircraft Industries, Ltd.) Airplanes
Unsafe Condition: unsafe condition on these products.
Why matched: Airworthiness Directives; Gulfstream Aerospace LP (Type Certificate Previously Held by Israel Aircraft Industries, Ltd.) Airplanes
2026-16-08 Recurring
final ruleAirworthiness Directives; Rolls-Royce Deutschland Ltd & Co KG Engines
Unsafe Condition: Cracking of the intermediate pressure (IP) compressor variable inlet guide vanes (VIGVs) due to high-cycle fatigue propagation.
Why matched: Airworthiness Directives; Rolls-Royce Deutschland Ltd & Co KG Engines
2026-17-09
final ruleAirworthiness Directives; Airbus SAS Airplanes
Unsafe Condition: Missing chamfers under the heads of critical fasteners on the primary structure of both pylons.
Why matched: Airworthiness Directives; Airbus SAS Airplanes
2026-18-03 Recurring
final ruleAirworthiness Directives; Airbus SAS Airplanes
Unsafe Condition: Tool mark damage in the bore of the forward and aft lugs of the main landing gear (MLG) support rib 5 due to a quality escape in production assembly.
Why matched: Airworthiness Directives; Airbus SAS Airplanes
2026-18-01
final ruleAirworthiness Directives; ATR-GIE Avions de Transport Régional Airplanes
Unsafe Condition: unsafe condition on these products.
Why matched: Airworthiness Directives; ATR-GIE Avions de Transport Régional Airplanes
2026-16-06 Recurring
final ruleAirworthiness Directives; The Boeing Company Airplanes
Unsafe Condition: Fatigue cracking in the lower outboard wing skin at the inboard fastener of stringer L-9.5 and the lower outboard wing skin of stringer L-6.5 on airplanes with winglets installed per STC ST01920SE.
Why matched: Airworthiness Directives; The Boeing Company Airplanes
2026-16-04
final ruleAirworthiness Directives; Airbus Helicopters
Unsafe Condition: The determination that new or more restrictive airworthiness limitations are necessary.
Why matched: Airworthiness Directives; Airbus Helicopters
2026-16-03 Recurring
final ruleAirworthiness Directives; Airbus Helicopters
Unsafe Condition: Cracks in the legs of the side supports of the tail rotor transmission fan.
Why matched: Airworthiness Directives; Airbus Helicopters
2026-16-05
final ruleAirworthiness Directives; Airbus Helicopters
Unsafe Condition: Magnetization on the solenoid valves for the three main servo-controls, the regulator block, and the tail servo-control due to a diode not properly installed in the hydraulic circuit.
Why matched: Airworthiness Directives; Airbus Helicopters
2026-17-10
final ruleAirworthiness Directives; Lycoming Engines
Unsafe Condition: Piston pin failure resulting in metal particulate contamination in the engine oil and engine failure.
Why matched: Airworthiness Directives; Lycoming Engines