AD 98-06-39

final rule
Data completeness: 70%

Airworthiness Directives; Eurocopter France Model AS 332C, L, L1, and L2 Helicopters

AD Number
98-06-39
Status
final_rule
Effective Date
Product Category
aircraft
Docket
97-SW-66-AD
FR Citation
Federal Register: March 20, 1998 (Volume 63, Number 54)

Applicability

TypeManufacturerModelDetails
aircraft Airbus Helicopters AS332C Airworthiness Directives; Eurocopter France Model AS 332C, L, L1, and L2 Helicopters
aircraft Airbus Helicopters AS332L Airworthiness Directives; Eurocopter France Model AS 332C, L, L1, and L2 Helicopters
aircraft Airbus Helicopters AS332L1 Airworthiness Directives; Eurocopter France Model AS 332C, L, L1, and L2 Helicopters
aircraft Airbus Helicopters AS332L2 Airworthiness Directives; Eurocopter France Model AS 332C, L, L1, and L2 Helicopters

Unsafe Condition

Cracked hinge tenons due to improper shimming of the cockpit door tenons, which may lead to door separation and impact with main or tail rotor systems, causing loss of control.

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

Required Actions

Inspect shim washer thickness and perform specified actions per Eurocopter Service Bulletin 01.00.50. Depending on washer thickness, inspect for cracks, replace hinge tenons if cracks are found before further flight, and reinstall with zero hours TIS hinge tenon within 500 hours time-in-service.

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

Compliance Time

Within 50 hours time-in-service (TIS)

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

Affected Aircraft

Eurocopter France Model AS 332C, L, L1, and L2 helicopters, certificated in any category.

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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