AD 98-06-36
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus Helicopters | SA341G | Airworthiness Directives; Eurocopter France Model SA341G and SA342J Helicopters |
| aircraft | Airbus Helicopters | SA342J | Airworthiness Directives; Eurocopter France Model SA341G and SA342J Helicopters |
Unsafe Condition
The unsafe condition could occur if the main rotor blade pitch change mechanism fails, leading to loss of control during flight.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect the main rotor blade pitch change mechanism for cracks or deformation, and replace any affected components found during the inspection.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
within 150 flight hours after the effective date of this AD
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Eurocopter France Model SA341G and SA342J helicopters with certain main rotor blade pitch change mechanisms as specified in the AD.
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
This site is not affiliated with or endorsed by the FAA. Always verify with official sources.