AD 2010-14-18
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Boeing | Company Model 767-200 | Airworthiness Directives; The Boeing Company Model 767-200, -300, and -300F Series Airplanes Powered by General Electric or Pratt & Whitney Engines |
Unsafe Condition
Fatigue cracking in the primary strut structure and reduced structural integrity of the strut, which could result in separation of the strut and engine.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect the eight aft-most fastener holes in the horizontal tangs of the midspar fitting of the strut for discrepancies. Inspect for cracks in the closeout angle that covers the two aft-most fasteners in the lower tang of the midspar fitting. Perform investigative and corrective actions if necessary. Reduce repetitive inspection intervals to 400 flight cycles and 6,000 flight cycles, depending on the inspection type.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 400 flight cycles since the previous inspection, or within 8,000 total flight cycles for airplanes that have not yet been inspected.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
The Boeing Company Model 767-200, -300, and -300F series airplanes powered by General Electric or Pratt & Whitney engines.
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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