AD 2000-16-07
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | Industrie Model A300 B2 and B4 | Airworthiness Directives; Airbus Industrie Model A300 B2 and B4 Series Airplanes |
Unsafe Condition
Bonding delamination and cracking of the fuselage longitudinal lap joints, circumferential joints, stringers, and doublers, which could result in rapid decompression of the airplane.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect fuselage longitudinal lap joints and circumferential joints for bonding delamination and corrosion/cracks, and repair as necessary. Inspect stringers and doublers for debonding and repair as necessary. Expand inspection areas, revise inspection thresholds or intervals, and modify certain longitudinal lap joints as specified.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 6 months after May 13, 1985, or as indicated by the applicable service bulletins.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Airbus Industrie Model A300 B2 and B4 series airplanes, manufacturer serial numbers 003 through 156 inclusive, certificated in any category.
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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