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99-01-02

final rule

Airworthiness Directives; Westland Helicopters Ltd. 30 Series 100 and 100-60 Helicopters

Unsafe Condition: Failure of the conformal pinion quill shafts installed in certain main rotor gearboxes (MRGB) could result in a forced landing or loss of control of the helicopter due to shock loading from slam en...

Effective: Jan 14, 1999 Category: aircraft Compliance: Prior to further flight

Why matched: Airworthiness Directives; Westland Helicopters Ltd. 30 Series 100 and 100-60 Helicopters

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

98-07-11

final rule

Airworthiness Directives; GKN Westland Helicopters Limited WG-30 Series 100 and 100-60 Helicopters

Unsafe Condition: Failure of a main rotor tie-bar due to bulging or swelling caused by water ingress into the blade sleeve, leading to loss of a main rotor blade and subsequent loss of control of the helicopter.

Effective: Apr 16, 1998 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; GKN Westland Helicopters Limited WG-30 Series 100 and 100-60 Helicopters

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

Amdt-39-10431

final rule

Airworthiness Directives; GKN Westland Helicopters Limited WG-30 Series 100 and 100-60 Helicopters

Unsafe Condition: Failure of a main rotor head tie-bar due to exceeding power-off transient rotor speed limitations could result in loss of a main rotor blade and subsequent loss of control of the helicopter.

Effective: Apr 16, 1998 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; GKN Westland Helicopters Limited WG-30 Series 100 and 100-60 Helicopters

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

98-06-06

final rule

Airworthiness Directives; GKN Westland Helicopters Ltd., 30 Series Helicopters

Unsafe Condition: Failure of the tail rotor drive shaft coupling attachment flanges due to cracks, which could result in loss of power to the tail rotor and subsequent loss of control of the helicopter.

Effective: Mar 31, 1998 Category: aircraft Compliance: Within

Why matched: Airworthiness Directives; GKN Westland Helicopters Ltd., 30 Series Helicopters

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

85-07-06

final rule

Airworthiness Directives; WESTLAND HELICOPTERS LIMITED Model 30 Helicopters

Unsafe Condition: Cracking of the main rotor blade sleeve tie-bar pin and possible loss of a main rotor blade

Effective: Apr 9, 1985 Category: aircraft Compliance: Within 50 hours time in service after the effective date of this AD or prior to attaining 500 hou...

Why matched: Airworthiness Directives; WESTLAND HELICOPTERS LIMITED Model 30 Helicopters

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

84-12-51

final rule

Airworthiness Directives; WESTLAND HELICOPTERS LIMITED Model 30 Series 100 Helicopter

Unsafe Condition: Cracking of the main rotor blades could cause possible hazards in flight.

Effective: Sep 11, 1984 Category: aircraft Compliance: Before next flight and thereafter before first flight of each day for visual inspections; within ...

Why matched: Airworthiness Directives; WESTLAND HELICOPTERS LIMITED Model 30 Series 100 Helicopter

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

84-01-52 R1

final rule

Airworthiness Directives; WESTLAND HELICOPTERS LIMITED Model 30 Series 100 Helicopters

Unsafe Condition: Failure of the tail rotor gearbox input pitch control lever and subsequent loss of control in flight.

Effective: Apr 16, 1984 Category: aircraft Compliance: Prior to further flight

Why matched: Airworthiness Directives; WESTLAND HELICOPTERS LIMITED Model 30 Series 100 Helicopters