AD 2022-03-13
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | Helicopters Model AS332L2 | Airworthiness Directives; Airbus Helicopters |
| aircraft | Aviat | Various | Airworthiness Directives; Airbus Helicopters |
Unsafe Condition
cracks on the two front attachment points of the support, and subsequent investigations determined pilot actions on the yaw pedals could generate detrimental loading conditions on the support attachment points and initiate a crack.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
repetitively inspect the support at the four attachment points for a crack, and if there is a crack, replace the support before further flight, or modify the helicopter by replacing an affected part with an improved part, which is a terminating action for the repetitive inspections.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 100 hours TIS after the effective date of this AD, and thereafter at intervals not exceeding 825 hours TIS.
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Affected Aircraft
Airbus Helicopters Model AS332L2 helicopters with a support part number (P/N) 332A25-1334-00 installed.
AI-generated summary from the source AD text. Verify against the official source before acting.
Source: Official FAA Source ↗
Retrieved: Apr 6, 2026
Rights: U.S. Government Public Domain
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