Airworthiness directives › 2025-07-08
AD 2025-07-08 Airworthiness Directives; Airbus Helicopters
Models named: AS332C, AS332C1, AS332L, AS332L1. Read the applicability below — it usually turns on serial or part numbers too.
Applicability*9
This AD applies to all Airbus Helicopters Model AS332C, AS332C1, AS332L, and AS332L1 helicopters. certificated in any category.
Compliance
Comply with this AD within the compliance times specified, unless already done.
Required actions
Except as specified in paragraph (h) of this AD: Comply with all required actions and compliance times specified in, and in accordance with European Union Aviation Safety Agency (EASA) AD 2025-0001, dated January 6, 2025 (EASA AD 2025-0001).
Unsafe condition
This AD was prompted by a report of the loss of the tail rotor pitch control. The FAA is issuing this AD to detect and address any score, scratch, crack, or corrosion on the slide of the control plate of the tail rotor head assembly. The unsafe condition, if not addressed, could result in structural failure of the tail rotor head assembly and reduced or loss of control of the helicopter.
Affected ADs
None.
Read the original on the Federal Register →
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The directive text above is reproduced from the Federal Register, a work of the United States government and in the public domain. The separation into applicability, compliance and required actions is TrackAD's.*1