AD 2008-05-10
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Boeing | 757-200 | Airworthiness Directives; Boeing Model 757-200, -200PF, and -200CB Series Airplanes |
| engine | Rolls-Royce | engines | Airworthiness Directives; Boeing Model 757-200, -200PF, and -200CB Series Airplanes |
Unsafe Condition
Cracks, loose and broken bolts, and shim migration in the joint between the aft torque bulkhead and the strut-to-diagonal brace fitting could result in damage to the strut and consequent separation of the strut and engine from the airplane.
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Required Actions
Inspect the shim installation between the vertical flange and bulkhead, and repair if necessary. Inspect for cracking of the four critical fastener holes in the horizontal flange, and repair if necessary. Perform these actions on airplanes without conclusive records of previous inspections.
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Compliance Time
Before further flight
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Affected Aircraft
Boeing Model 757-200, -200PF, and -200CB series airplanes powered by Rolls-Royce engines.
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Source: Official FAA Source ↗
Retrieved: Apr 4, 2026
Rights: U.S. Government Public Domain
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