AD 2000-07-26
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A300 | Airworthiness Directives; Airbus Model A300 Series Airplanes |
Unsafe Condition
Corrosion on the outer surface of the fuselage skin panel, which could result in cracking and consequent reduced structural integrity of the airplane.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Perform a one-time detailed visual inspection of the fuselage skin panel between fuselage frames FR39 and FR40, and between stringers 27 and 33, for corrosion. Apply corrosion preventive protection. Repair or replace corroded areas as necessary, in accordance with Airbus Service Bulletin A300-53-0328, Revision 01.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 6, 12, or 18 months after the effective date of the AD, depending on the airplane's date of manufacture.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Airbus Model A300 series airplanes, certificated in any category, except those on which Airbus Modification 04201 has been accomplished.
AI-generated summary from the source AD text. Verify against the official source before acting.
Source: Official FAA Source ↗
Retrieved: Apr 6, 2026
Rights: U.S. Government Public Domain
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