AD 2005-04-14
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Boeing | 757-200 | Airworthiness Directives; Boeing Model 757-200, 757-200CB, and 757-200PF Series Airplanes Equipped With Rolls Royce Model RB211 Engines |
Unsafe Condition
Migration of shims at the joint of the mid-bulkhead and the upper link fittings, and cracking of the mid-bulkhead, which could result in cracking of the strut and consequent loss of the strut and engine.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect for horizontal or vertical movement of the shims at the joint of the mid-bulkhead and the upper link fittings, and take corrective action if necessary. Decrease the allowable tolerance for shim migration. Perform repetitive detailed inspections for cracking of the entire mid-bulkhead, and repair if necessary.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 90 days of the effective date of this AD for a one-time detailed inspection for cracking, followed by repetitive detailed inspections.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Boeing Model 757-200, 757-200CB, and 757-200PF series airplanes equipped with Rolls Royce Model RB211 engines.
AI-generated summary from the source AD text. Verify against the official source before acting.
Source: Official FAA Source ↗
Retrieved: Apr 4, 2026
Rights: U.S. Government Public Domain
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