2026-20-15 Recurring
final ruleAirworthiness Directives; Airbus SAS Airplanes
Unsafe Condition: unsafe condition on these products.
Why matched: Airworthiness Directives; Airbus SAS Airplanes
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3,144 results found (771ms)
2026-21-03 Recurring
final ruleAirworthiness Directives; Airbus SAS Airplanes
Unsafe Condition: unsafe condition on these products.
Why matched: Airworthiness Directives; Airbus SAS Airplanes
2026-20-08
final ruleAirworthiness Directives; Airbus Helicopters
Unsafe Condition: The tail rotor drive fan wheels and impeller second stage have been incorrectly identified during production.
Why matched: Airworthiness Directives; Airbus Helicopters
2026-20-03
final ruleAirworthiness Directives; Airbus Helicopters
Unsafe Condition: The instructions on how to open the sliding door emergency exit are insufficient.
Why matched: Airworthiness Directives; Airbus Helicopters
2026-20-05 Recurring
final ruleAirworthiness Directives; Airbus SAS Airplanes
Unsafe Condition: unsafe condition on these products.
Why matched: Airworthiness Directives; Airbus SAS Airplanes
2026-19-02
final ruleAirworthiness Directives; Airbus Helicopters
Unsafe Condition: Main rotor blades (MRB) not certified for installation on the helicopters, leading to lack of instructions for continued airworthiness and improper maintenance.
Why matched: Airworthiness Directives; Airbus Helicopters
2026-21-02 Recurring
final ruleAirworthiness Directives; Airbus Helicopters Deutschland GmbH (AHD) Helicopters
Unsafe Condition: unsafe condition on these products.
Why matched: Airworthiness Directives; Airbus Helicopters Deutschland GmbH (AHD) Helicopters
2026-18-09 Recurring
final ruleAirworthiness Directives; Airbus SAS Airplanes
Unsafe Condition: Cracked and broken restraint brackets of the anti-ice piccolo tube found during maintenance on certain nacelle inlet cowls.
Why matched: Airworthiness Directives; Airbus SAS Airplanes
2026-20-06
final ruleAirworthiness Directives; Airbus Helicopters Deutschland GmbH (AHD) Helicopters
Unsafe Condition: Loss of oil from the main gearbox (MGB) may not activate the low pressure caution or warning light.
Why matched: Airworthiness Directives; Airbus Helicopters Deutschland GmbH (AHD) Helicopters
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
2026-17-01
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
2026-17-04 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
2026-16-10 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
2026-17-09
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
2026-16-04
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
2026-16-01
final ruleAirworthiness Directives; Airbus Helicopters
Unsafe Condition: An incorrectly installed engine flange on the main gear box (MGB) engine coupling.
Why matched: Airworthiness Directives; Airbus Helicopters
2026-15-14
final ruleAirworthiness Directives; Airbus Canada Limited Partnership (Type Certificate Previously Held by C Series Aircraft Limited Partnership (CSALP); Bombardier, Inc.) Airplanes
Unsafe Condition: Engine bleed duct large leak condition may occur, requiring manual isolation of the opposite functional engine.
Why matched: Airworthiness Directives; Airbus Canada Limited Partnership (Type Certificate Previously Held by C Series Aircraft Limited Partnership (CSALP); Bombardier, Inc.) Airplanes
2026-15-10 Recurring
final ruleAirworthiness Directives; Airbus SAS Airplanes
Unsafe Condition: Crack findings on the sloping rib.
Why matched: Airworthiness Directives; Airbus SAS Airplanes
2026-15-01
final ruleAirworthiness Directives; Airbus SAS Airplanes
Unsafe Condition: The oxygen supply from a single oxygen cylinder is insufficient for ETOPS-180 operations with four flightcrew members.
Why matched: Airworthiness Directives; Airbus SAS Airplanes
2026-15-13 Recurring
final ruleAirworthiness Directives; Airbus SAS Airplanes
Unsafe Condition: Repetitive replacement of the high-pressure bleed valve (HPV) clips is necessary to address the unsafe condition.
Why matched: Airworthiness Directives; Airbus SAS Airplanes
2026-14-04 Recurring
final ruleAirworthiness Directives; Airbus SAS Airplanes
Unsafe Condition: The unsafe condition involves the potential installation of affected parts that could lead to failure of the broadband antenna adapter plate, skirt, vents, and attachment fittings.
Why matched: Airworthiness Directives; Airbus SAS Airplanes
2026-14-05
final ruleAirworthiness Directives; Airbus SAS Airplanes
Unsafe Condition: Dual loss of radio management panel (RMP) data synchronization
Why matched: Airworthiness Directives; Airbus SAS Airplanes