AD 2010-05-03
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Boeing | Company Model 747-100 | Airworthiness Directives; The Boeing Company Model 747-100, 747-100B, 747-100B SUD, 747-200B, 747-200C, 747-200F, 747-300, 747-400, 747-400D, 747-400F, 747SR, and 747SP Series Airplanes |
Unsafe Condition
Fatigue cracking in the wing and horizontal stabilizer side-of-body joints, and the fuselage skin circumferential splices, due to high cyclic loads, could connect to form large cracks and result in reduced structural integrity leading to rapid decompression and consequent loss of control of the airplane.
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Required Actions
Perform one-time detailed and high frequency eddy current inspections for cracks in the wing and horizontal stabilizer side-of-body joints and the fuselage skin circumferential splices, and repair if necessary. For certain airplanes, perform repetitive detailed inspections for cracks of the fuselage skin circumferential splices, and repair if necessary. Report positive findings to Boeing.
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Compliance Time
Within 28,500 to 30,000 total flight cycles or 130,000 to 135,000 total flight hours, whichever occurs later.
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Affected Aircraft
The Boeing Company Model 747-100, 747-100B, 747-100B SUD, 747-200B, 747-200C, 747-200F, 747-300, 747-400, 747-400D, 747-400F, 747SR, and 747SP series airplanes.
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Source: Official FAA Source ↗
Retrieved: Apr 4, 2026
Rights: U.S. Government Public Domain
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