AD Amdt-39-9644
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A300 B2 and B4 | Airworthiness Directives; Airbus Model A300 B2 and B4 Series Airplanes, Excluding Model A300-600 Series Airplanes |
Unsafe Condition
Stress corrosion cracking in the skin at the longitudinal lap joint at certain stringers of the fuselage caused by increased stress levels from rework beyond specified limits.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Measure the thickness of the inner skin of the longitudinal lap joint from the inside of the fuselage at certain stringers. Inspect for stress corrosion cracking in the subject area and repair if necessary.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Before further flight
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Affected Aircraft
Airbus Model A300 B2 and B4 series airplanes, excluding Model A300-600 Series.
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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