AD 2005-13-30
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Boeing | 737-100 | Airworthiness Directives; Boeing Model 737-100, -200, and -200C Series Airplanes |
Unsafe Condition
Fatigue cracking of fuselage skin panels just aft of the main wheelwell, which could cause rapid decompression of the airplane.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect unmodified fuselage side skins just aft of the main wheelwell before the airplane accumulates 16,000 total flight cycles or within 4,500 flight cycles after the effective date of the AD, whichever occurs later. For modified skin areas, inspect as specified in Boeing Service Bulletin 737-53-1065, Revision 2. Repair any detected cracking, loose fasteners, disbonding, or damage before further flight.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Before the airplane accumulates 16,000 total flight cycles or within 4,500 flight cycles after the effective date of the AD, whichever occurs later.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
All Boeing Model 737-100, -200, and -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 6, 2026
Rights: U.S. Government Public Domain
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