AD 99-10-06
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Textron Aviation Inc. | 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 ribs, which could propagate to the trailing edge of the wing and cause the panel to separate from the wing during flight.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Immediately incorporate temporary revisions to the AFM Limitations Section prohibiting flap operation during takeoff and requiring preflight visual inspections of the aft cove panel for delamination. Repetitively inspect the trailing edge of the wing cove skin panels for delamination and modify the center flap track rib attachment when delamination is found. Incorporate repair schemes using specified service information.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Immediately
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Raytheon Model Beech 2000 airplanes, serial numbers NC-4 through NC-53, without Raytheon Kit 122-4019, Rev. B incorporated.
AI-generated summary from the source AD text. Verify against the official source before acting.
Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
This site is not affiliated with or endorsed by the FAA. Always verify with official sources.