AD Amdt-39-11160
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Raytheon | Aircraft Corporation Model Beech 2000 | Airworthiness Directives; Raytheon Aircraft Corporation Model Beech 2000 Airplanes |
Unsafe Condition
Delamination of the wing cove skin panel in the area of the support rib, which could propagate to the trailing edge and result in the wing cove skin panel separating from the wing during flight.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Revise the AFM Limitations Section to prohibit flap operation during takeoff. Perform preflight visual inspections of the aft cove panel for delamination. Incorporate a repair scheme if delamination is found. Repeatedly inspect the trailing edge of the wing for delamination. Modify the center flap track rib attachment if delamination is detected.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Immediately
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Affected Aircraft
Raytheon Aircraft Corporation Model Beech 2000 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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