AD 2017-17-01
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | Various | Airworthiness Directives; Airbus Helicopters |
Unsafe Condition
Corrosion or a crack in an attachment pin, which could result in loss of a main rotor (M/R) blade 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
Inspect each attachment pin for corrosion, cracks, and pitting. Replace the attachment pin if there is a crack or any pitting. Remove corrosion up to a maximum of four times. Inspect the protective coating of each attachment pin.
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 AS332L2 helicopters with attachment pin part numbers 332A31-2123-00 or 332A31-2115-20 installed, and Model EC225LP helicopters with attachment pin part number 332A31-3204-20 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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