AD 2005-20-03
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Boeing | 737-100 | Airworthiness Directives; Boeing Model 737-100, -200, -200C, -300, -400, and -500 Series Airplanes |
Unsafe Condition
Fatigue cracks in the intercostal webs, attachment clips, and stringer splice channels on the forward and aft sides of the forward entry door, which could result in loss of the forward entry door and rapid decompression of the airplane.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Conduct repetitive inspections of the intercostal webs, attachment clips, and stringer splice channels for cracks. Take corrective action if cracks are found.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 4,500 flight cycles after the effective date of the AD.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Boeing Model 737-100, -200, -200C, -300, -400, and -500 series 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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