AD 98-13-39

final rule
Data completeness: 70%

Airworthiness Directives; Eurocopter France Model AS 332C, L, and L1 Helicopters

AD Number
98-13-39
Status
final_rule
Effective Date
Product Category
aircraft
Docket
97-SW-39-AD
FR Citation
Federal Register: June 26, 1998 (Volume 63, Number 123)

Applicability

TypeManufacturerModelDetails
aircraft Airbus Helicopters AS332C Airworthiness Directives; Eurocopter France Model AS 332C, L, and L1 Helicopters
aircraft Airbus Helicopters AS332L Airworthiness Directives; Eurocopter France Model AS 332C, L, and L1 Helicopters
aircraft Airbus Helicopters AS332L1 Airworthiness Directives; Eurocopter France Model AS 332C, L, and L1 Helicopters

Unsafe Condition

Cracks on the tail rotor shaft flapping hinge retainers (part number 330A33.3165.00) could lead to high tail rotor vibrations, loss of tail rotor control, and subsequent loss of control of the helicopter.

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

Required Actions

Perform a dye penetrant inspection of each retainer before further flight and before the first flight of each day. Replace any retainer found cracked with an airworthy retainer.

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

Compliance Time

Prior to further flight, and thereafter before the first flight of each day.

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

Affected Aircraft

Eurocopter France Model AS 332C, L, and L1 helicopters with tail rotor shaft flapping hinge retainer, part number 330A33.3165.00, installed.

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

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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