AD 2006-05-02
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Boeing | 747-200F | Airworthiness Directives; Boeing Model 747-200F, 747-200C, 747-400, 747-400D, and 747-400F Series Airplanes |
Unsafe Condition
Fatigue cracks can occur in certain fuselage internal structure, potentially leading to loss of structural integrity and rapid depressurization.
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Required Actions
Perform initial and repetitive inspections for fuselage cracks using specified methods, and repair all cracks as detailed in Boeing Alert Service Bulletin 747-53A2500.
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Compliance Time
Within the times specified in the Accomplishment Instructions of Boeing Alert Service Bulletin 747-53A2500.
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Affected Aircraft
All Boeing Model 747-200F, 747-200C, 747-400, 747-400D, and 747-400F series airplanes, certificated in any category.
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Source: Official FAA Source ↗
Retrieved: Apr 6, 2026
Rights: U.S. Government Public Domain
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