AD 2021-03-01
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | Helicopters Model AS332C | Airworthiness Directives; Airbus Helicopters |
| aircraft | Aviat | Various | Airworthiness Directives; Airbus Helicopters |
Unsafe Condition
Failure of a tail rotor flapping hinge could result in unbalance of the tail rotor, detachment of the tail rotor gearbox and hub, and subsequent loss of control of the helicopter.
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Required Actions
Comply with all required actions and compliance times specified in, and in accordance with, European Union Aviation Safety Agency (EASA) AD 2020-0086, dated April 14, 2020 (EASA AD 2020-0086).
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Compliance Time
Within 25 hours time-in-service after the effective date of this AD.
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Affected Aircraft
All Airbus Helicopters Model AS332C, AS332C1, AS332L, AS332L1, and SA330J helicopters, certificated in any category, all manufacturer serial numbers.
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Source: Official FAA Source ↗
Retrieved: Apr 4, 2026
Rights: U.S. Government Public Domain
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