AD 99-11-03
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus Helicopters | SA341G | Airworthiness Directives; Eurocopter France Model SA341G and SA342J |
| aircraft | Airbus Helicopters | SA342J | Airworthiness Directives; Eurocopter France Model SA341G and SA342J |
Unsafe Condition
Corrosion affecting the main rotor head pitch-change rod (rod), which could lead to failure of the rod 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
Before further flight, visually inspect the external body of each rod for corrosion. If external corrosion is found, inspect the inside of the body for corrosion. Replace rods with external corrosion exceeding repair criteria or any internal corrosion with an airworthy rod. Additionally, inspect inside of each rod within 10 hours time-in-service or 7 calendar days, whichever occurs first, if not previously done.
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Compliance Time
Before further flight
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Affected Aircraft
Eurocopter France Model SA341G and SA342J helicopters, certificated in any category.
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Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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