AD Amdt-39-11468
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Boeing | 767 | Airworthiness Directives; Boeing Model 767 Series Airplanes |
Unsafe Condition
Fatigue cracking of end cap bolts caused by improper installation, which could lead to failure of the end cap assembly and separation of the engine from the airplane in the event of a primary thrust linkage failure.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Accomplish initial and repetitive inspections of the forward engine mount to ensure the proper condition of the engine thrust link components. Replace the end cap assembly with an improved assembly within 3 years after the effective date of the AD. Repair any discrepancies found during inspections prior to further flight.
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Compliance Time
Within 3 years after the effective date of the AD.
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Affected Aircraft
Boeing Model 767 series airplanes, powered by Pratt & Whitney Model JT9D or Model PW4000 series engines, as listed in Boeing Alert Service Bulletin 767-71A0087, dated October 10, 1996; 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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