AD 2005-07-08
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Boeing | 757-200 and -200PF | Airworthiness Directives; Boeing Model 757-200 and -200PF Series Airplanes |
Unsafe Condition
Delamination of the leading edge slats, possible loss of pieces of the trailing edge wedge assembly during flight, reduction of maneuver and stall margins, and consequent reduced controllability of the airplane.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect and perform audible tap tests of the upper and lower skins of the trailing edge wedges on certain slats. Investigate and take corrective actions if necessary. Optional terminating action is provided for repetitive inspections and tap tests.
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Compliance Time
Within 18 months of the effective date of the AD.
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Affected Aircraft
Boeing Model 757-200 and -200PF series airplanes, certificated in any category, with line numbers 1 through 139 inclusive, as identified in Boeing Alert Service Bulletin 757-57A0063, dated June 26, 2003.
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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