Bell Helicopter Textron Canada Limited Airworthiness Directives

475 ADs indexed for Bell Helicopter Textron Canada Limited aircraft.

Models

206A 70 ADs 206B 61 ADs 206L 49 ADs 206L-1 49 ADs 205A-1 49 ADs 212 44 ADs 206L-3 40 ADs 204B 32 ADs 222 31 ADs 206B-1 30 ADs 222B 30 ADs 206A-1 (OH-58A) 29 ADs 407 28 ADs 222U 28 ADs 205A 27 ADs 412 26 ADs 206L-4 25 ADs 214ST 25 ADs 214B 22 ADs 214B-1 22 ADs 430 20 ADs 205B 20 ADs 230 18 ADs 412EP 15 ADs 427 12 ADs 429 12 ADs 412CF 9 ADs Various 5 ADs 204B 5 ADs 210 5 ADs 505 4 ADs 412 3 ADs 412CF 3 ADs 412EP 3 ADs AB412 3 ADs AB412 EP 3 ADs Various 3 ADs 412 2 ADs 412CF 2 ADs 412EP 2 ADs AB412 2 ADs AB412 EP 2 ADs TH-1F 2 ADs TH-1L 2 ADs UH-1A 2 ADs UH-1B 2 ADs UH-1E 2 ADs UH-1F 2 ADs UH-1H 2 ADs UH-1L 2 ADs UH-1P 2 ADs 206 2 ADs 206A 2 ADs 206B 2 ADs 206L 2 ADs 206L-1 2 ADs 206L-3 2 ADs 206L-4 2 ADs 222 2 ADs 222B 2 ADs 222U 2 ADs 230 2 ADs 407 2 ADs 427 2 ADs 430 2 ADs 204B 1 AD 205A 1 AD 205A-1 1 AD TH-1L 1 AD UH-1B 1 AD UH-1E 1 AD UH-1F 1 AD UH-1L 1 AD TH-1L 1 AD UH-1A 1 AD UH-1B 1 AD UH-1E 1 AD UH-1F 1 AD UH-1L 1 AD 205A 1 AD 205A-1 1 AD 205B 1 AD 212 1 AD High Landing Gear Aft Crosstube Assembly 1 AD High landing gear forward crosstube assembly 1 AD A318-111 1 AD A318-112 1 AD A318-121 1 AD A318-122 1 AD A319-111 1 AD A319-112 1 AD A319-113 1 AD A319-114 1 AD A319-115 1 AD AW139 1 AD 212 1 AD 214B 1 AD 214B-1 1 AD 214ST 1 AD 412 1 AD 412CF 1 AD 412EP 1 AD 429 1 AD 430 1 AD A109 1 AD A109A 1 AD A109A II 1 AD A109C 1 AD A109E 1 AD A109K2 1 AD A109S 1 AD AB139 1 AD AB412 1 AD AB412 EP 1 AD AS-365N3 1 AD AS332L2 1 AD AW109SP 1 AD AW139 1 AD EC135P1 1 AD EC135P2 1 AD EC135P2+ 1 AD EC135T1 1 AD EC135T2 1 AD EC135T2+/EC635T2+ 1 AD EC225LP 1 AD MBB-BK 117 C-2 1 AD MD900 1 AD S-61L 1 AD S-61N 1 AD S-61NM 1 AD S-61R 1 AD S-70 1 AD S-70A 1 AD S-70C 1 AD S-70C(M) 1 AD S-70C(M1) 1 AD S-76A 1 AD S-76B 1 AD S-76C 1 AD S-76D 1 AD S-92A 1 AD 206 1 AD 206A 1 AD 206A-1 (OH-58A) 1 AD A109 1 AD A109A 1 AD A109A II 1 AD A109C 1 AD A109E 1 AD A109K2 1 AD A109S 1 AD 206A 1 AD 206B 1 AD 206L 1 AD 206L-1 1 AD 206L-3 1 AD 206L-4 1 AD 210 1 AD 212 1 AD 407 1 AD 412 1 AD 412CF 1 AD 412EP 1 AD 427 1 AD AB412 1 AD AB412 EP 1 AD BO-105A 1 AD BO-105C 1 AD BO-105LS A-1 1 AD BO-105LS A-3 1 AD BO-105S 1 AD EC135P1 1 AD EC135P2 1 AD EC135P2+ 1 AD EC135T1 1 AD EC135T2 1 AD EC135T2+/EC635T2+ 1 AD 205A 1 AD 205A-1 1 AD 205B 1 AD 212 1 AD 206A 1 AD 206B 1 AD 206L 1 AD 206L-1 1 AD 206L-3 1 AD 206L-4 1 AD 407 1 AD AS350B 1 AD AS350B1 1 AD AS350B2 1 AD AS350B3 1 AD AS350BA 1 AD AS350C 1 AD AS350D 1 AD AS350D1 1 AD EC130B4 1 AD A300 B2-1A 1 AD A300 B2-1C 1 AD A300 B2-203 1 AD A300 B2K-3C 1 AD A300 B4-103 1 AD A300 B4-203 1 AD A300 B4-2C 1 AD A300 B4-601 1 AD A300 B4-603 1 AD A300 B4-605R 1 AD 204B 1 AD 205A 1 AD 205A-1 1 AD SW205A-1 1 AD TH-1L 1 AD UH-1A 1 AD UH-1B 1 AD UH-1E 1 AD UH-1F 1 AD UH-1H 1 AD UH-1L 1 AD AH-1S 1 AD HH-1K 1 AD TH-1F 1 AD TH-1L 1 AD UH-1A 1 AD UH-1B 1 AD UH-1E 1 AD UH-1F 1 AD UH-1H 1 AD UH-1L 1 AD UH-1P 1 AD HH-1K 1 AD TH-1F 1 AD TH-1L 1 AD UH-1A 1 AD UH-1B 1 AD UH-1E 1 AD UH-1F 1 AD UH-1H 1 AD UH-1L 1 AD UH-1P 1 AD HH-1K 1 AD SW204HP (UH-1B) 1 AD SW205A-1 1 AD TH-1F 1 AD TH-1L 1 AD UH-1A 1 AD UH-1B 1 AD UH-1E 1 AD UH-1F 1 AD UH-1H 1 AD UH-1L 1 AD UH-1P 1 AD Various 1 AD 172 1 AD 172A 1 AD 172B 1 AD 172C 1 AD 172D 1 AD 172E 1 AD 172F (USAF T-41A) 1 AD 172G 1 AD 172H (USAF T-41A) 1 AD 407 1 AD 150G 1 AD 172H (USAF T-41A) 1 AD 180H 1 AD 182J 1 AD 182K 1 AD 185E 1 AD 188 1 AD 206A 1 AD 210F 1 AD 210G 1 AD 206 1 AD 206A 1 AD 206A-1 (OH-58A) 1 AD 206B 1 AD 206B-1 1 AD 206L 1 AD 206L-1 1 AD 206L-3 1 AD 206L-4 1 AD Auxiliary Fuel System 1 AD 205B 1 AD 412 1 AD 204B 1 AD 205A 1 AD 205A-1 1 AD 205B 1 AD 209/AH-1G 1 AD 210 1 AD 212 1 AD AH-1S 1 AD HH-1K 1 AD SW204 (UH-1B) 1 AD SW204HP (UH-1B) 1 AD SW205 (UH-1H) 1 AD SW205A-1 1 AD TH-1F 1 AD TH-1L 1 AD UH-1A 1 AD UH-1B 1 AD UH-1E 1 AD UH-1F 1 AD UH-1H 1 AD UH-1L 1 AD UH-1P 1 AD 222 1 AD 222B 1 AD 222U 1 AD AS355E 1 AD AS355F 1 AD AS355F1 1 AD AS355F2 1 AD BO-105A 1 AD BO-105C 1 AD BO-105LS A-1 1 AD BO-105LS A-3 1 AD BO-105S 1 AD MBB-BK 117 A-1 1 AD MBB-BK 117 A-3 1 AD MBB-BK 117 A-4 1 AD MBB-BK 117 B-1 1 AD TH-1L 1 AD UH-1A 1 AD UH-1B 1 AD UH-1E 1 AD UH-1F 1 AD UH-1H 1 AD UH-1L 1 AD 204B 1 AD 205A 1 AD 205A-1 1 AD 205B 1 AD 212 1 AD UH-1B 1 AD UH-1F 1 AD UH-1H 1 AD TH-1L 1 AD UH-1E 1 AD UH-1L 1 AD HH-1K 1 AD TH-1F 1 AD TH-1L 1 AD UH-1A 1 AD UH-1B 1 AD UH-1E 1 AD UH-1F 1 AD UH-1H 1 AD UH-1L 1 AD UH-1P 1 AD HH-1K 1 AD TH-1F 1 AD TH-1L 1 AD UH-1A 1 AD UH-1B 1 AD UH-1E 1 AD UH-1F 1 AD UH-1H 1 AD UH-1L 1 AD UH-1P 1 AD HH-1K 1 AD TH-1F 1 AD TH-1L 1 AD UH-1A 1 AD UH-1B 1 AD UH-1E 1 AD UH-1F 1 AD UH-1H 1 AD UH-1L 1 AD UH-1P 1 AD HH-1K 1 AD SW204HP (UH-1B) 1 AD SW205A-1 1 AD TH-1F 1 AD TH-1L 1 AD UH-1A 1 AD UH-1B 1 AD UH-1E 1 AD UH-1F 1 AD UH-1H 1 AD UH-1L 1 AD UH-1P 1 AD HH-1K 1 AD SW205A-1 1 AD TH-1F 1 AD TH-1L 1 AD UH-1A 1 AD UH-1B 1 AD UH-1E 1 AD UH-1F 1 AD UH-1H 1 AD UH-1L 1 AD UH-1P 1 AD HH-1K 1 AD TH-1F 1 AD TH-1L 1 AD UH-1A 1 AD UH-1B 1 AD UH-1E 1 AD UH-1F 1 AD UH-1H 1 AD UH-1L 1 AD UH-1P 1 AD HH-1K 1 AD TH-1F 1 AD TH-1L 1 AD UH-1A 1 AD UH-1B 1 AD UH-1E 1 AD UH-1F 1 AD UH-1H 1 AD UH-1L 1 AD UH-1P 1 AD HH-1K 1 AD SW204HP (UH-1B) 1 AD SW205A-1 1 AD TH-1F 1 AD TH-1L 1 AD UH-1A 1 AD UH-1B 1 AD UH-1E 1 AD UH-1F 1 AD UH-1H 1 AD UH-1L 1 AD UH-1P 1 AD HH-1K 1 AD SW204 (UH-1B) 1 AD SW204HP (UH-1B) 1 AD SW205 (UH-1H) 1 AD SW205A-1 1 AD TH-1F 1 AD TH-1L 1 AD UH-1A 1 AD UH-1B 1 AD UH-1E 1 AD UH-1F 1 AD UH-1H 1 AD UH-1L 1 AD UH-1P 1 AD HH-1K 1 AD SW204HP (UH-1B) 1 AD SW205A-1 1 AD TH-1F 1 AD TH-1L 1 AD UH-1A 1 AD UH-1B 1 AD UH-1E 1 AD UH-1F 1 AD UH-1H 1 AD UH-1L 1 AD UH-1P 1 AD HH-1K 1 AD SW204HP (UH-1B) 1 AD SW205A-1 1 AD TH-1F 1 AD TH-1L 1 AD UH-1A 1 AD UH-1B 1 AD UH-1E 1 AD UH-1F 1 AD UH-1H 1 AD UH-1L 1 AD UH-1P 1 AD

Recent ADs

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

2022-23-02 Recurring

final rule

Airworthiness Directives; Bell Textron Canada Limited (Type Certificate Previously Held by Bell Helicopter Textron Canada Limited) Helicopters

Unsafe Condition: A report of a crack on the tailboom lower skin due to fatigue damage, which could affect the structural integrity of the tailboom.

Effective: Jan 3, 2023 Category: aircraft Compliance: Before further flight

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

2022-22-08 Recurring

final rule

Airworthiness Directives; Bell Textron Canada Limited (Type Certificate Previously Held by Bell Helicopter Textron Canada Limited) Helicopters

Unsafe Condition: delamination of M/R blades

Effective: Dec 23, 2022 Category: aircraft Compliance: Within 50 flight hours

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

2022-09-07

final rule

Airworthiness Directives; Bell Textron Canada Limited (Type Certificate Previously Held by Bell Helicopter Textron Canada Limited) Helicopters

Unsafe Condition: The condition, if not addressed, could result in pitch link failure and subsequent loss of control of the helicopter.

Effective: May 31, 2022 Category: aircraft Compliance: Within 50 flight hours

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

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

2022-06-20 Recurring

final rule

Airworthiness Directives; Bell Textron Canada Limited (Type Certificate Previously Held by Bell Helicopter Textron Canada Limited) Helicopters

Unsafe Condition: The condition, if not addressed, could result in restrictions in the collective, directional, or pitch control systems, and subsequent loss of helicopter control.

Effective: Apr 26, 2022 Category: aircraft Compliance: Within 12 months after the helicopter was manufactured or 30 days after the effective date of thi...

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

Technical illustration of an aircraft flight control surface and actuator
Problem area Flight controls

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

2022-02-02

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

2021-24-04

final rule

Airworthiness Directives; Bell Textron Canada Limited (Type Certificate Previously Held by Bell Helicopter Textron Canada Limited) Helicopters

Unsafe Condition: unsatisfactory flight performance of the engine above pressure altitude limitations for Jet B and JP-4 fuels, which could result in low fuel pressure, engine flame-out, or engine power interruption.

Effective: Jan 13, 2022 Category: aircraft Compliance: Within 30 calendar days after the effective date of this AD

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

2021-20-11 Recurring

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Airworthiness Directives; Bell Textron Canada Limited (Type Certificate Previously Held by Bell Helicopter Textron Canada Limited) Helicopters

Unsafe Condition: Reports of incorrectly staked spherical bearings in the directional control bellcrank assembly, which could result in wear or elongation of the bore in the bellcrank, and reduced helicopter directi...

Effective: Nov 22, 2021 Category: aircraft Compliance: Within 50 flight hours

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

2021-18-16 Recurring

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Airworthiness Directives; Bell Textron Canada Limited (Type Certificate Previously Held by Bell Helicopter Textron Canada Limited) Helicopters

Unsafe Condition: tail rotor gearbox assemblies found loose on the gearbox support, which could result in structural damage and possible loss of control of the helicopter

Effective: Nov 1, 2021 Category: aircraft Compliance: Within 12 months after the effective date

Why matched: Airworthiness Directives; Bell Textron Canada Limited (Type Certificate Previously Held by Bell Helicopter Textron Canada Limited) 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

2021-15-06

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Airworthiness Directives; Bell Textron Canada Limited (Type Certificate Previously Held by Bell Helicopter Textron Canada Limited)

Unsafe Condition: Operating a helicopter with the affected tail rotor disc assembly could result in loss of control of the helicopter.

Effective: Aug 27, 2021 Category: aircraft Compliance: Within 50 flight hours

Why matched: Airworthiness Directives; Bell Textron Canada Limited (Type Certificate Previously Held by Bell Helicopter Textron Canada Limited)

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

2021-15-51

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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

2021-13-15

final rule

Airworthiness Directives; Bell Textron Canada Limited (Type Certificate Previously Held by Bell Helicopter Textron Canada Limited) Helicopters

Unsafe Condition: unsafe condition on these products.

Effective: Jul 29, 2021 Category: aircraft

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

2021-11-19

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Airworthiness Directives; Bell Textron Canada Limited (Type Certificate Previously Held by Bell Helicopter Textron Canada Limited) Helicopters

Unsafe Condition: A gap between the transmission restraint assembly aft attachment hardware lower washer and the mating airframe truss assembly (truss assembly) clevis lower lug.

Effective: Jul 16, 2021 Category: aircraft Compliance: Within 100 hours time-in-service (TIS)

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

2021-10-08

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Airworthiness Directives; Bell Textron Canada Limited (Type Certificate Previously Held by Bell Helicopter Textron Canada Limited) Helicopters

Unsafe Condition: a manufacturing flaw that could cause a switch unit to hang in the high position and fail to indicate a low fuel condition

Effective: Jun 11, 2021 Category: aircraft Compliance: Within 100 hours after the effective date of this AD

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

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

2021-03-13

final rule

Airworthiness Directives; Bell Textron Canada Limited (Type Certificate Previously Held by Bell Helicopter Textron Canada Limited) Helicopters

Unsafe Condition: Failure to observe the CFB life limit could result in excessive vibration and loss of control of the helicopter.

Effective: Apr 1, 2021 Category: aircraft Compliance: Within 50 hours time-in-service

Why matched: Airworthiness Directives; Bell Textron Canada Limited (Type Certificate Previously Held by Bell Helicopter Textron Canada Limited) 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

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