AD 2004-13-06
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A319 and A320 | Airworthiness Directives; Airbus Model A319 and A320 Series Airplanes |
Unsafe Condition
Fatigue cracks on the side panels of the keel beams, which could result in reduced structural integrity of the airplane.
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Required Actions
Perform a detailed inspection to detect cracks in the keel beam side panels, in accordance with Airbus Service Bulletin A320-53-1060, Revision 01. Repeat the inspection at intervals not to exceed 4,300 flight cycles or 9,600 flight hours. Repair any cracks found in 'Area A' or 'Area B' before further flight, as specified.
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Compliance Time
Within 3,500 flight cycles after the effective date of the AD.
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Affected Aircraft
Airbus Model A319 and A320 series airplanes, certificated in any category, except those airplanes on which Airbus Modification 30355 has been incorporated in production.
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Source: Official FAA Source ↗
Retrieved: Apr 4, 2026
Rights: U.S. Government Public Domain
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