AD 2001-07-05
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Boeing | 767 | Airworthiness Directives; Boeing Model 767 Series Airplanes Powered by General Electric or Pratt & Whitney Engines |
| engine | Pratt & Whitney | engines | Airworthiness Directives; Boeing Model 767 Series Airplanes Powered by General Electric or Pratt & Whitney Engines |
Unsafe Condition
Fatigue cracking in primary strut structure and reduced structural integrity of the strut, which could result in separation of the strut and engine.
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Required Actions
Conduct repetitive inspections to detect discrepancies of the aft-most fastener holes in the horizontal tangs of the midspar fitting of the strut. Perform corrective actions if necessary. Optional terminating action for repetitive inspections is provided.
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Compliance Time
Within 600 flight hours or 1,500 flight cycles, depending on prior inspections per Boeing Service Bulletin 767-54A0101, Revision 1.
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Affected Aircraft
Boeing Model 767 series airplanes powered by General Electric or Pratt & Whitney engines.
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Source: Official FAA Source ↗
Retrieved: Apr 6, 2026
Rights: U.S. Government Public Domain
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