AD Amdt-39-10942
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A310 | Airworthiness Directives; Airbus Model A310 Series Airplanes |
Unsafe Condition
Fatigue cracks at certain locations on the fuselage, horizontal stabilizer, and wings and tail, which could reduce structural integrity and potentially lead to failure of structural members or accelerate cracking of other structural members.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect for fatigue cracks at specified locations on the fuselage, horizontal stabilizer, and wings and tail. Repair or modify as necessary. Install doublers where required. Add new inspections and reduce certain inspection intervals.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 50 flight hours after the effective date of the AD.
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Affected Aircraft
All Airbus Model A310 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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