AD 2000-02-10
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Boeing | 747 | Airworthiness Directives; Boeing Model 747 Series Airplanes |
Unsafe Condition
Fatigue cracks at the inner chord and web of the body station 1265 edge frame between stringers 23 and 27, which could result in rapid depressurization of the airplane.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect for broken fasteners and cracking of the forward edge frame for main entry door number 3. Repair any detected cracking, if necessary.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Repetitive inspections as specified in the AD.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Boeing Model 747 series airplanes, as specified in the AD.
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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