AD 2011-04-06
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A340-200 | Airworthiness Directives; Airbus Model A340-200, -300, -500, and -600 Series Airplanes |
| aircraft | Aviat | Various | Airworthiness Directives; Airbus Model A340-200, -300, -500, and -600 Series Airplanes |
Unsafe Condition
Fatigue cracking, damage, and corrosion in certain structure, which could result in reduced structural integrity of the airplane.
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Required Actions
Revise operator maintenance documents to include new inspections as specified in Airbus A340 ALI Document AI/SE-M4/95A.0051/97, Issue 11. Compliance with these inspections is required by 14 CFR 91.403(c). Operators with previously modified, altered, or repaired areas may need to request approval for an alternative method of compliance.
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Compliance Time
Within the applicable maintenance intervals specified in Airbus A340 ALI Document AI/SE-M4/95A.0051/97, Issue 11.
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Affected Aircraft
Airbus Model A340-200, -300, -500, and -600 Series Airplanes, including A340-211, -212, -213, -311, -312, -313, -541, and -642 airplanes, all manufacturer serial numbers.
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Source: Official FAA Source ↗
Retrieved: Apr 6, 2026
Rights: U.S. Government Public Domain
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