AD 2016-23-01
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A310 | Airworthiness Directives; Airbus Airplanes |
Unsafe Condition
Fatigue cracking around the fastener holes in wing top skin panels between the front and rear spars on the left- and right-hand sides of the fuselage, particularly at ribs 2 and 3, could result in reduced structural integrity of the airplane.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect wing top skin panels 1 and 2 at ribs 2 and 3 for cracking around fastener holes, using detailed inspections and supplemental repetitive ultrasonic inspections. Repair any detected cracking as necessary.
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.
AI-generated summary from the source AD text. Verify against the official source before acting.
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 4, 2026
Rights: U.S. Government Public Domain
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