AD 2003-07-08

Recurring final rule
Data completeness: 70%

Airworthiness Directives; Boeing Model 757-200, 757-200CB, and 757-200PF Series Airplanes

AD Number
2003-07-08
Status
final_rule
Effective Date
Product Category
engine
Docket
Docket No. 2002-NM-315-AD
FR Citation
68 FR 16200

Applicability

TypeManufacturerModelDetails
aircraft Boeing 757-200 Airworthiness Directives; Boeing Model 757-200, 757-200CB, and 757-200PF Series Airplanes

Unsafe Condition

Migration of shims at the joint of the mid-bulkhead and the upper link fittings 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

Conduct repetitive detailed inspections to detect 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. Alternatively, perform certain alternative actions to terminate the requirement for repetitive inspections.

AI-generated summary from the source AD text. Verify against the official source before acting.

Compliance Time

Before further flight

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Affected Aircraft

Boeing Model 757-200, 757-200CB, and 757-200PF series airplanes.

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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