AD 2025-07-08
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | Helicopters Model AS332C | Airworthiness Directives; Airbus Helicopters |
| aircraft | Aviat | Various | Airworthiness Directives; Airbus Helicopters |
Unsafe Condition
Loss of tail rotor pitch control due to fracture of the tail rotor slide of the TRH assembly.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect the slide of the control plate of the TRH assembly for score, scratch, crack, or corrosion. Remove corrosion and replace the TRH assembly, slide of the control plate, or pitch control assembly if discrepancies are found. Report inspection results to Airbus Helicopters.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Before further flight
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Airbus Helicopters Model AS332C, AS332C1, AS332L, and AS332L1 helicopters.
AI-generated summary from the source AD text. Verify against the official source before acting.
Source: Official FAA Source ↗
Retrieved: Apr 4, 2026
Rights: U.S. Government Public Domain
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