AD 2004-15-07
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A310 | Airworthiness Directives; Airbus Model A310 Series Airplanes |
Unsafe Condition
Fatigue cracking of the area around the fasteners of the landing plate of the aileron access doors and the bottom skin panel of the wings, which could result in reduced structural integrity of the wings.
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Required Actions
Conduct repetitive high frequency eddy current (HFEC) inspections for cracking of the area around the fasteners of the landing plate of the wing bottom skin panel No. 2 of the left and right wings, as specified in Airbus Service Bulletin A310-57-2082. If cracking is found, perform a permanent repair per the Accomplishment Instruction of Airbus Service Bulletin A310-57-2082 or take the optional terminating action per Airbus Service Bulletin A310-57-2081.
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Compliance Time
Within 2,000 flight cycles after the effective date of this AD, or within 3,000 flight cycles after the last inspection done per paragraph (k) of AD 98-26-01, amendment 39-10942, whichever is first. Subsequent inspections must be conducted at intervals not to exceed 1,900 flight cycles.
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Affected Aircraft
Airbus Model A310 series airplanes, certificated in any category, on which Airbus Modification 12525 has not been done during production.
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Source: Official FAA Source ↗
Retrieved: Apr 6, 2026
Rights: U.S. Government Public Domain
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