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26 results found (772ms)

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2025-07-01

final rule

Airworthiness Directives; Thommen Aircraft Equipment AG Digital Air Data Computers

Unsafe Condition: Occurrences of AC32 Digital ADCs that stopped functioning due to the power module failing at temperatures below -20 degrees Celsius.

Effective: May 15, 2025 Category: aircraft Compliance: Within 12 months after the effective date of this AD

Why matched: Airworthiness Directives; Thommen Aircraft Equipment AG Digital Air Data Computers

2024-20-07 Recurring

final rule

Airworthiness Directives; Various Helicopters

Unsafe Condition: Difficulty pulling the emergency float kit activation handle installed on the pilot cyclic, and deficiencies in the installation of the cables on the emergency float kits.

Effective: Dec 5, 2024 Category: aircraft Compliance: Within 50 flight hours

Why matched: Airworthiness Directives; Various Helicopters

2024-16-19 Recurring

final rule

Airworthiness Directives; Bell Textron Inc. Helicopters

Unsafe Condition: Cracked tail boom attachment barrel nuts (barrel nuts) due to corrosion damage, high time in service, or hydrogen embrittlement, which can cause loss of torque on the associated bolt and subsequent...

Effective: Nov 8, 2024 Category: aircraft Compliance: Within 5,000 flight hours or 5 years, depending on the specific helicopter model and serial number.

Why matched: Airworthiness Directives; Bell Textron Inc. Helicopters

2024-17-02

final rule

Airworthiness Directives; Bell Textron Inc. Helicopters

Unsafe Condition: Failure of the tail boom attachment structure, including fatigue cracking of tail boom attachment fittings, cap angles, longerons, and bolts.

Effective: Nov 8, 2024 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; Bell Textron Inc. Helicopters

2024-19-17

final rule

Airworthiness Directives; Bell Textron Inc. and Various Restricted Category Helicopters

Unsafe Condition: The failure of a tension torsion (TT) strap, which can result in loss of a main rotor blade and subsequent loss of control of the helicopter.

Effective: Oct 11, 2024 Category: aircraft Compliance: Within 50 hours time-in-service (TIS)

Why matched: Airworthiness Directives; Bell Textron Inc. and Various Restricted Category Helicopters

Technical illustration of a helicopter rotor hub assembly
Problem area Rotor system

2024-16-01 Recurring

final rule

Airworthiness Directives; Bell Textron Inc. (Type Certificate Previously Held by Bell Helicopter Textron, Inc.), Helicopters

Unsafe Condition: The unsafe condition is a fatigue crack in a tail boom attachment cap angle, which can lead to failure of the cap angle, loss of the tail boom, and subsequent loss control of the helicopter.

Effective: Sep 4, 2024 Category: aircraft Compliance: Within 25 flight hours for certain helicopters and 50 flight hours for certain other helicopters

Why matched: Airworthiness Directives; Bell Textron Inc. (Type Certificate Previously Held by Bell Helicopter Textron, Inc.), Helicopters

2023-11-07

final rule

Airworthiness Directives; Various Helicopters

Unsafe Condition: unsafe condition on these products.

Effective: Jun 22, 2023 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; Various Helicopters

2022-20-14 Recurring

final rule

Airworthiness Directives; Bell Textron Inc., Helicopters and Various Restricted Category Helicopters

Unsafe Condition: Stress corrosion cracking of the main transmission support case lateral mounts.

Effective: Dec 27, 2022 Category: aircraft Compliance: Within 300 hours time-in-service (TIS) after accumulating 6,000 or more total hours TIS, or befor...

Why matched: Airworthiness Directives; Bell Textron Inc., Helicopters and Various Restricted Category Helicopters

2022-22-12

final rule

Airworthiness Directives; Bell Textron Inc., Erickson 214 Holdings, LLC, Leonardo S.p.a., and Various Restricted Category Helicopters

Unsafe Condition: Reports of two in-service failures of forward crosstubes due to fatigue damage, and the issuance of newly established life limits.

Effective: Nov 22, 2022 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; Bell Textron Inc., Erickson 214 Holdings, LLC, Leonardo S.p.a., and Various Restricted Category Helicopters

2022-21-11 Recurring

final rule

Airworthiness Directives; Bell Textron Inc. Helicopters and Various Restricted Category Helicopters

Unsafe Condition: Cracked main rotor blades (MRBs) with chordwise cracks originating from the extreme trailing edge between blade station 190 and 210.

Effective: Nov 16, 2022 Category: aircraft Compliance: Before the first flight of each day, and at 25-hour intervals, or within 12 months of effective d...

Why matched: Airworthiness Directives; Bell Textron Inc. Helicopters and Various Restricted Category Helicopters

Technical illustration of a helicopter rotor hub assembly
Problem area Rotor system

2022-11-19 Recurring

final rule

Airworthiness Directives; Bell Textron Inc. Helicopters

Unsafe Condition: A cracked check valve may exist on certain Bell Textron Inc. Model 212, 412, 412CF, and 412EP helicopters with an engine oil check valve part number (P/N) 209-062-520-001 or fuel check valve P/N 20...

Effective: Jul 6, 2022 Category: engine Compliance: Within 25 hours TIS or 30 days, whichever occurs first after the effective date of this AD

Why matched: Airworthiness Directives; Bell Textron Inc. Helicopters

Technical illustration of an aircraft turbine engine assembly
Problem area Engine

2022-07-02

final rule

Airworthiness Directives; Bell Textron Inc. Helicopters

Unsafe Condition: A crack in the spar cap, if not detected and corrected, could create stress concentrations at the edge of the rivet holes, resulting in reduced structural integrity of the helicopter and subsequent...

Effective: May 9, 2022 Category: aircraft Compliance: Within 100 hours time-in-service (TIS) after the effective date of this AD, and thereafter at int...

Why matched: Airworthiness Directives; Bell Textron Inc. Helicopters

2022-07-03

final rule

Airworthiness Directives; Bell Textron Inc., Helicopters

Unsafe Condition: The condition, if not addressed, could result in fatigue damage and cracking, failure of the collective lever, and subsequent loss of control of the helicopter.

Effective: Apr 27, 2022 Category: aircraft Compliance: Within 50 hours TIS after the effective date of this AD

Why matched: Airworthiness Directives; Bell Textron Inc., Helicopters

2022-05-10 Recurring

final rule

Airworthiness Directives; Goodrich Externally-Mounted Hoist Assemblies

Unsafe Condition: The overload clutch in the Goodrich externally-mounted hoist assemblies can fail, leading to in-flight loss of the hoist load, possibly resulting in injury to persons on the ground or in a hoisting...

Effective: Apr 20, 2022 Category: aircraft Compliance: Within 12 months of effective date

Why matched: Airworthiness Directives; Goodrich Externally-Mounted Hoist Assemblies

2022-06-03

final rule

Airworthiness Directives; Bell Textron Inc. (Type Certificate Previously Held by Bell Helicopter Textron Inc.) Helicopters

Unsafe Condition: The affected pin may shear off during flight, resulting in the main rotor blade and the main rotor head detaching from the helicopter.

Effective: Mar 16, 2022 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; Bell Textron Inc. (Type Certificate Previously Held by Bell Helicopter Textron Inc.) Helicopters

Technical illustration of a helicopter rotor hub assembly
Problem area Rotor system

2022-06-05

final rule

Airworthiness Directives; Various Restricted Category Helicopters

Unsafe Condition: Failure of a pin could result in the main rotor blade detaching from the helicopter and subsequent loss of control of the helicopter.

Effective: Mar 16, 2022 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; Various Restricted Category Helicopters

Technical illustration of a helicopter rotor hub assembly
Problem area Rotor system

2022-02-02

final rule

Airworthiness Directives; Bell Textron Inc. (Type Certificate Previously Held by Bell Helicopter Textron Inc.) Helicopters

Unsafe Condition: This AD was prompted by a fatal accident in which a pin sheared off during flight, which resulted in the main rotor blade and the main rotor head detaching from the helicopter.

Effective: Feb 16, 2022 Category: aircraft Compliance: Before further flight from August 24, 2021 (the effective date of AD 2021-15-51), for Model 204B,...

Why matched: Airworthiness Directives; Bell Textron Inc. (Type Certificate Previously Held by Bell Helicopter Textron Inc.) Helicopters

Technical illustration of a helicopter rotor hub assembly
Problem area Rotor system

2021-20-02

final rule

Airworthiness Directives; Bell Textron Inc. (Type Certificate Previously Held by Bell Helicopter Textron Inc.) Helicopters

Unsafe Condition: The unsafe condition, if not addressed, could result in fatigue and failure of the grip assembly and loss of helicopter control.

Effective: Oct 28, 2021 Category: aircraft Compliance: Within 50 flight hours

Why matched: Airworthiness Directives; Bell Textron Inc. (Type Certificate Previously Held by Bell Helicopter Textron Inc.) Helicopters

2021-15-14 Recurring

final rule

Airworthiness Directives; Various Restricted Category Helicopters

Unsafe Condition: Failure of the tail boom attach structure, including the bolts, resulting in separation of the tail boom from the helicopter and subsequent loss of control of the helicopter.

Effective: Aug 30, 2021 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; Various Restricted Category Helicopters

2021-15-51

final rule

Airworthiness Directives; Bell Textron Inc. (Type Certificate Previously Held by Bell Helicopter Textron Inc.) Helicopters

Unsafe Condition: A pin P/N 204-012-104-005 with an S/N prefix 'FNFS' sheared off during flight, resulting in the main rotor blade and the main rotor head detaching from the helicopter. The pin had accumulated only ...

Effective: Aug 24, 2021 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; Bell Textron Inc. (Type Certificate Previously Held by Bell Helicopter Textron Inc.) Helicopters

Technical illustration of a helicopter rotor hub assembly
Problem area Rotor system

2021-04-19

final rule

Airworthiness Directives; Bell Textron Inc. (Type Certificate Previously Held by Bell Helicopter Textron Inc.) Helicopters

Unsafe Condition: The T/R blades sustain greater loads when used on Bell Model 205B helicopters compared to their use on other model helicopters, resulting in failure of the T/R blade and subsequent loss control of ...

Effective: Apr 13, 2021 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; Bell Textron Inc. (Type Certificate Previously Held by Bell Helicopter Textron Inc.) Helicopters

2020-22-07

final rule

Airworthiness Directives; Bell Textron Inc. (Type Certificate Previously Held by Bell Helicopter Textron Inc.) Helicopters

Unsafe Condition: excessive pylon pitch vibrations likely caused overload that resulted in cracked main gearbox (MGB) support case failures, and investigations are ongoing to determine the root cause of these vibrat...

Effective: Nov 18, 2020 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; Bell Textron Inc. (Type Certificate Previously Held by Bell Helicopter Textron Inc.) Helicopters

2020-19-08

final rule

Airworthiness Directives; Bell Textron Inc. (Type Certificate Previously Held by Bell Helicopter Textron Inc.) Helicopters

Unsafe Condition: Corrosion detected on main rotor hub tension-torsion strap (TT strap) assemblies.

Effective: Oct 21, 2020 Category: aircraft Compliance: Within 25 hours time-in-service (TIS)

Why matched: Airworthiness Directives; Bell Textron Inc. (Type Certificate Previously Held by Bell Helicopter Textron Inc.) Helicopters

Technical illustration of a helicopter rotor hub assembly
Problem area Rotor system

2020-16-10

final rule

Airworthiness Directives; Bell Textron Inc. (Type Certificate Previously Held by Bell Helicopter Textron Inc.) Helicopters

Unsafe Condition: a comfort clip interfering with the seat belt inertia reel

Effective: Sep 3, 2020 Category: aircraft Compliance: Within 50 hours time-in-service

Why matched: Airworthiness Directives; Bell Textron Inc. (Type Certificate Previously Held by Bell Helicopter Textron Inc.) Helicopters

2020-14-01

final rule

Airworthiness Directives; Bell Textron Inc. (Type Certificate Previously Held by Bell Helicopter Textron Inc.) Helicopters

Unsafe Condition: The discovery that bolts have nonconforming external thread root radii. The unsafe condition, if not addressed, could result in the spindle separating from the yoke and subsequent loss of control o...

Effective: Aug 11, 2020 Category: aircraft Compliance: Within 25 hours time-in-service

Why matched: Airworthiness Directives; Bell Textron Inc. (Type Certificate Previously Held by Bell Helicopter Textron Inc.) Helicopters