AD 2002-19-08
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Vulcanair | S.p.A. P 68 Series | Airworthiness Directives; Vulcanair S.p.A. P 68 Series Airplanes |
Unsafe Condition
Failure of the primary flight control system caused by incorrect connecting bolt and linkage installation, interference, or incorrect installation of certain components.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect the flight and engine control systems for correct connecting bolt and linkage installation, no interference, and correct installation of certain components. Make necessary adjustments and modify/install the split link and full travel limit assembly.
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
Vulcanair S.p.A. P 68 series airplanes.
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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