AD 2005-01-18
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Raytheon | Aircraft Company Beech 100 | Airworthiness Directives; Raytheon Aircraft Company Beech 100, 200, and 300 Series Airplanes |
Unsafe Condition
Cracks in fuselage stringers (Nos. 5 through 11) in the rear pressure bulkhead area could result in structural damage to the fuselage, leading to fuselage failure and potential loss of control of the airplane.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect fuselage stringers (Nos. 5 through 11) in the rear pressure bulkhead area for cracks. Repair any cracked fuselage stringers. No operation is allowed for airplanes with five or more cracked stringers until modification is completed. For airplanes with less than five cracked stringers, operation is allowed for up to 25 hours time-in-service (TIS) before repair is required.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 25 hours time-in-service (TIS) for airplanes with less than five cracked stringers; before further flight for airplanes with five or more cracked stringers.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Raytheon Aircraft Company Beech 100, 200, and 300 series airplanes, including specific models and serial numbers as listed in the AD: A100-1 (U-21J), 200 and B200, A200 (C-12A) and A200 (C-12C), A200C (UC-12B), and others within the specified serial ranges.
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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