AD 2025-13-10
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | SAS | Airworthiness Directives; Airbus SAS Airplanes |
Unsafe Condition
Fatigue cracking may occur in affected areas on airplanes having Sharklets installed during production or in service.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect the left-hand and right-hand wing manhole access panel attachment holes in the bottom wing skin panels 2, between rib 13 and rib 23, for cracks. If any cracks are found, repair the affected area in accordance with the instructions in the Airbus Structural Repair Manual (SRM).
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Compliance Time
Within 50 flight hours after the effective date of this AD
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Affected Aircraft
Airbus SAS Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes; Model A320-211, -212, -214, -216, -231, -232, and -233 airplanes; and Model A321-111, -112, -131, -211, -212, -213, -231, and -232 airplanes.
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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