Bell Helicopter Textron Inc. Airworthiness Directives

30 ADs indexed for Bell Helicopter Textron Inc. aircraft.

Models

Recent ADs

2022-06-03

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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

2021-20-02

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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

2021-15-51

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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

2021-04-19

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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

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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

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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

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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

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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

2020-02-11

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Airworthiness Directives; Bell Helicopter Textron Inc. Helicopters

Unsafe Condition: Numerous failures of inverters due to an external connector that caused a short circuit inside inverter P/N 412-375-079-101 and components chafing because of variations in the assembly process and ...

Effective: Mar 17, 2020 Category: aircraft Compliance: Within 25 hours time-in-service (TIS)

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

Technical illustration of an aircraft electrical generator and wiring assembly
Problem area Electrical system

2018-16-14

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Airworthiness Directives; Bell Helicopter Textron Inc., Helicopters

Unsafe Condition: A crack on an EFS tube assembly could result in failure of the emergency floats to inflate during an emergency water landing.

Effective: Oct 4, 2018 Category: aircraft Compliance: Within 300 hours time-in-service

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

2015-04-04

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Airworthiness Directives; Bell Helicopter Textron Inc. Helicopters

Unsafe Condition: Failure of an inverter(s) under instrument meteorological conditions or night flight, which could result in smoke in the cockpit, increased pilot workload due to the loss of primary flight and navi...

Effective: Mar 11, 2015 Category: aircraft Compliance: Within 5 hours time-in-service

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

2014-03-10

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Airworthiness Directives; Various Restricted Category Helicopters

Unsafe Condition: An incorrectly machined body on the cable assembly could prevent the barrel assembly from fully engaging in the body cavity, leading to disengagement of the cable from the barrel, failure of the ta...

Effective: Mar 26, 2014 Category: aircraft Compliance: Within 50 hours time in service

Why matched: Airworthiness Directives; Various Restricted Category Helicopters

2013-13-06

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Airworthiness Directives; Various Restricted Category Helicopters

Unsafe Condition: Cracks originating in the lower main rotor blade bolt lug, attributed to subsurface fatigue, corrosion, and mechanical damage, leading to grip failure and potential main rotor blade separation.

Effective: Sep 10, 2013 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

2013-13-14

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Airworthiness Directives; Various Restricted Category Helicopters

Unsafe Condition: Cracking in main rotor hub inboard strap fittings, which may lead to fitting failure, loss of a main rotor blade, and subsequent loss of helicopter control.

Effective: Jul 24, 2013 Category: aircraft Compliance: Within 25 hours TIS or 15 days, whichever comes first.

Why matched: Airworthiness Directives; Various Restricted Category Helicopters

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

2012-26-11

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Airworthiness Directives; Bell Helicopter Textron Inc. Helicopters

Unsafe Condition: The power cable assembly connector deterioration can cause a short in the connector, potentially leading to a fire in the starter/generator, smoke in the cockpit, reduced visibility, and risk of lo...

Effective: Feb 13, 2013 Category: aircraft Compliance: Within six months

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

Technical illustration of an aircraft electrical generator and wiring assembly
Problem area Electrical system

2012-17-10

final rule

Airworthiness Directives; Various Restricted Category Helicopters

Unsafe Condition: Fatigue cracks on main rotor (M/R) blades installed on Bell Helicopter Textron, Inc. (Bell) Model 212 helicopters, specifically in the lower skin, doublers, and box beam at the M/R blade attachment...

Effective: Sep 28, 2012 Category: aircraft Compliance: Within 25 hours time-in-service (TIS), and thereafter at intervals not to exceed 25 hours TIS.

Why matched: Airworthiness Directives; Various Restricted Category Helicopters

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

2012-14-12

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Airworthiness Directives; Various Restricted Category Helicopters

Unsafe Condition: Missing tail rotor blade tip blocks or tip closures due to adhesive bond voids or incorrect screw installation, leading to blade loss and potential helicopter loss of control.

Effective: Sep 4, 2012 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

2009-05-09

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Airworthiness Directives; Bell Helicopter Textron Inc. Model 412, 412CF, and 412EP Helicopters

Unsafe Condition: Fatigue cracking of a main rotor yoke, failure of a yoke, and subsequent loss of control of the helicopter.

Effective: Mar 31, 2009 Category: aircraft Compliance: Within 10 hours TIS for reidentification and record-keeping actions; before further flight for re...

Why matched: Airworthiness Directives; Bell Helicopter Textron Inc. Model 412, 412CF, and 412EP Helicopters

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

2006-19-05

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Airworthiness Directives; Arrow Falcon Exporters, Inc. (Previously Utah State University); Firefly Aviation Helicopter Services (Previously Erickson Air-Crane Co.); California Department of Forestry; Garlick Helicopters, Inc.; Global Helicopter Technology, Inc.; Hagglund Helicopters, LLC (Previously Western International Aviation, Inc.); International Helicopters, Inc.; Precision Helicopters, LLC; Robinson Air Crane, Inc.; San Joaquin Helicopters (Previously Hawkins and Powers Aviation, Inc.) S.M.&T. Aircraft (Previously U.S. Helicopters, Inc., UNC Helicopter, Inc., Southern Aero Corporation, and Wilco Aviation); Smith Helicopters; Southern Helicopter, Inc.; Southwest Florida Aviation International, Inc. (Previously Jamie R. Hill and Southwest Florida Aviation); Tamarack Helicopters, Inc. (Previously Ranger Helicopter Services, Inc.); U.S. Helicopter, Inc. (Previously UNC Helicopter, Inc.); West Coast Fabrication; and Williams Helicopter Corporation (Previously Scott Paper Co.) Model HH-1K, TH-1F, TH-1L, UH-1A, UH-1B, UH-1E, UH-1F, UH-1H, UH-1L, and UH-1P Helicopters; and Southwest Florida Aviation Model SW204, SW204HP, SW205, and SW205A-1 Helicopters

Unsafe Condition: This amendment adopts a new airworthiness directive (AD) for the specified restricted category type-certificated helicopters. The AD requires a review of the helicopter records to determine the Com...

Effective: Oct 16, 2006 Category: aircraft Compliance: before further flight

Why matched: Airworthiness Directives; Arrow Falcon Exporters, Inc. (Previously Utah State University); Firefly Aviation Helicopter Services (Previously Erickson Air-Crane Co.); California Department of Forestry; Garlick Helicopters, Inc.; Global Helicopter Technology, Inc.; Hagglund Helicopters, LLC (Previously Western International Aviation, Inc.); International Helicopters, Inc.; Precision Helicopters, LLC; Robinson Air Crane, Inc.; San Joaquin Helicopters (Previously Hawkins and Powers Aviation, Inc.) S.M.&T. Aircraft (Previously U.S. Helicopters, Inc., UNC Helicopter, Inc., Southern Aero Corporation, and Wilco Aviation); Smith Helicopters; Southern Helicopter, Inc.; Southwest Florida Aviation International, Inc. (Previously Jamie R. Hill and Southwest Florida Aviation); Tamarack Helicopters, Inc. (Previously Ranger Helicopter Services, Inc.); U.S. Helicopter, Inc. (Previously UNC Helicopter, Inc.); West Coast Fabrication; and Williams Helicopter Corporation (Previously Scott Paper Co.) Model HH-1K, TH-1F, TH-1L, UH-1A, UH-1B, UH-1E, UH-1F, UH- 1H, UH-1L, and UH-1P Helicopters; and Southwest Florida Aviation Model SW204, SW204HP, SW205, and SW205A-1 Helicopters

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

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