AD 2013-04-12
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A310-204 | Airworthiness Directives; Airbus Airplanes |
Unsafe Condition
Fatigue cracking of slat extension eccentric bolts, classified as principal structural elements (PSE), could result in the loss of structural integrity of the airplane.
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Required Actions
Replace slat extension eccentric bolts and associated washers with new parts as specified in Airbus Mandatory Service Bulletin A310-57-2100, Revision 01, dated February 3, 2012. The specific part numbers and locations are detailed in the AD.
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Compliance Time
Before the accumulation of specified total flight hours or flight cycles, depending on the model and average flight time (AFT).
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Affected Aircraft
Airbus Model A310-204, -222, -304, -322, and -324 airplanes, certificated in any category, having received in production Airbus modification 04809 without Airbus modification 06243 or 13596.
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Source: Official FAA Source ↗
Retrieved: Apr 6, 2026
Rights: U.S. Government Public Domain
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