AD 2006-12-17
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Boeing | 737-200C | Airworthiness Directives; Boeing Model 737-200C Series Airplanes |
Unsafe Condition
Cracking of the fuselage frames from body station (BS) 360 to BS 500B, which could lead to loss of the cargo door during flight and consequent rapid decompression of the airplane.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Perform a one-time external detailed inspection for cracks in the fuselage skin between stringers 19 left and 25 left and at BS 360 to BS 540. Perform repetitive internal detailed inspections for cracks of the frames between stringers 19 left and 25 left and at BS 360 to BS 500B. Repair all cracks as specified. Install doublers on the specified frames between stringers 19 left and 25 left from BS 360 to BS 500B.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within specified flight cycles as detailed in the AD.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
All Boeing Model 737-200C series airplanes, certificated in any category.
AI-generated summary from the source AD text. Verify against the official source before acting.
Source: Official FAA Source ↗
Retrieved: Apr 4, 2026
Rights: U.S. Government Public Domain
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