AD Amdt-39-10383

final rule
Data completeness: 70%

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

AD Number
Amdt-39-10383
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 97-SW-26-AD
FR Citation
63 FR 12607

Applicability

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

Unsafe Condition

Cracks in the tail rotor drive shaft attachment flanges could result in loss of power to the tail rotor and subsequent loss of control.

AI-generated summary from the source AD text. Verify against the official source before acting.

Required Actions

Determine the total hours time-in-service (TIS) of the six tail rotor drive shafts, create a component history card or equivalent record for each shaft, and replace drive shafts exceeding specified TIS with an airworthy one.

AI-generated summary from the source AD text. Verify against the official source before acting.

Compliance Time

Before further flight

AI-generated summary from the source AD text. Verify against the official source before acting.

Affected Aircraft

GKN Westland Helicopters Ltd. 30 series helicopters

AI-generated summary from the source AD text. Verify against the official source before acting.

Source: Official FAA Source ↗

Retrieved: Apr 6, 2026

Rights: U.S. Government Public Domain

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