AD 2010-22-03
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A310 | Airworthiness Directives; Airbus Model A310 Series Airplanes |
| aircraft | Aviat | Various | Airworthiness Directives; Airbus Model A310 Series Airplanes |
Unsafe Condition
Reduced structural integrity of the wings due to a structural fatigue phenomenon of the rear spar internal angle and the tee fitting located in the centre wing box.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect for cracks in the rear spar internal angle and the left and right sides of the tee fitting using repetitive rotating probe inspections. Modify the holes in the internal angle and tee fitting by cold expansion. Perform related investigative and corrective actions as necessary.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 60 months after June 7, 2006 (effective date of AD 2006-09-05), or as specified in the Accomplishment Instructions of Airbus Service Bulletin A310-57-2035, Revision 10, dated March 25, 2008.
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Affected Aircraft
All Airbus Model A310-203, -204, -221, -222, -304, -322, -324, and -325 airplanes, certificated in any category.
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Source: Official FAA Source ↗
Retrieved: Apr 6, 2026
Rights: U.S. Government Public Domain
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