AD 2026-01-05
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Boeing | Company | Airworthiness Directives; The Boeing Company Airplanes |
| aircraft | Aviat | Various | Airworthiness Directives; The Boeing Company Airplanes |
Unsafe Condition
The potential for cracking on the right- or left-wing lower stringer L-8 or L-6 vertical web flange at a fastener common to the reinforcement strap.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Perform a general visual inspection (GVI) or maintenance records check of certain stringers for an approved freeze plug repair, perform a high frequency eddy current (HFEC) inspection of the same area for any crack common to a certain stringer and a reinforcement strap, and applicable on-condition actions.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 50 flight hours
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
The Boeing Company Model 757-200 and -300 series airplanes, equipped with Aviation Partners Boeing (APB) scimitar blended winglets.
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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