AD Amdt-39-11005

final rule
Data completeness: 70%

Airworthiness Directives, Eurocopter France Model AS332C, L, and L1 Helicopters

AD Number
Amdt-39-11005
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 97-SW-41-AD
FR Citation
64 FR 4288

Unsafe Condition

Premature failure of main rotor hub spindles and flapping hinge pins due to increased loading from increased stiffness of aged frequency adapters.

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

Required Actions

Replace certain main rotor hub spindles and flapping hinge pins as specified in the AD.

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

Eurocopter France Model AS332C, L, and L1 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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View Official Source ↗