AD Amdt-39-9238
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Aerospatiale | Model ATR42-200, -300, and -320 Series | Airworthiness Directives; Aerospatiale Model ATR42-200, -300, and -320 Series Airplanes |
Unsafe Condition
Loss of a propeller and engine gearbox resulting in fuselage damage, and modification to elevator control cables reducing maximum physical separation between elevator controls and pitch trim dissymmetry monitoring equipment.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Modify the wiring in the elevator controls and pitch trim dissymmetry monitoring equipment to prevent reduced controllability due to debris strikes from engine burst or propeller failure.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Before further flight
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Affected Aircraft
Aerospatiale Model ATR42-200, -300, and -320 series airplanes with modifications to elevator control cables during manufacture.
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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