AD 2004-25-02
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A320 | Airworthiness Directives; Airbus Model A320 Series Airplanes |
Unsafe Condition
Fatigue cracking of the fuselage, which could result in reduced structural integrity of the airplane.
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Required Actions
Perform a detailed inspection to detect cracking on the outboard flanges around the fastener holes of frames 38 through 41, between stringers 12 and 21, using Airbus Service Bulletin A320-53-1032, Revision 02, dated December 5, 2001. The inspection intervals are reduced based on the airplane's inspection history and flight cycle counts.
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Compliance Time
Within specified flight cycles, depending on the airplane's inspection history and flight cycle counts.
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Affected Aircraft
Airbus Model A320-111, -211, -212, and -231 series airplanes on which Airbus Modification 21346 has not been done, 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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