AD 2007-20-03
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A300-600 | Airworthiness Directives; Airbus Model A300-600 Series Airplanes |
| aircraft | Aviat | Various | Airworthiness Directives; Airbus Model A300-600 Series Airplanes |
Unsafe Condition
Fatigue cracking, damage, or corrosion in principal structural elements, which could result in reduced structural integrity of the airplane.
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Required Actions
Revise the Airworthiness Limitations Section (ALS) of the Instructions for Continued Airworthiness to incorporate Airbus A300-600 Airworthiness Limitation Items (ALI) Document AI/SE-M2/95A.0502/06, Issue 11, dated April 2006.
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Compliance Time
Within 3 months after the effective date of this AD.
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Affected Aircraft
Airbus Model A300-600 series airplanes, all certified models, all serial numbers, certificated in any category.
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Source: Official FAA Source ↗
Retrieved: Apr 4, 2026
Rights: U.S. Government Public Domain
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