AD 2006-25-04
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A300 | Airworthiness Directives; Airbus Model A300 Airplanes |
Unsafe Condition
Corrosion and cracking in the lower rim area, service apertures, and upper rim area of the rear pressure bulkhead, as well as missing or damaged sealant in the area between the outer attachment angle and circumferential joint doubler, could lead to reduced structural capability of the fuselage and consequent decompression of the airplane.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect for cracking and corrosion in the lower rim area of the rear pressure bulkhead and adjacent areas, and in the service apertures and upper rim area of the rear pressure bulkhead. Inspect for missing or damaged sealant in the area between the outer attachment angle and circumferential joint doubler. Perform additional inspections for corrosion in certain areas and repetitive inspections for airplanes on which repairs have been done. Take corrective actions as necessary.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Before further flight for certain inspections; within specified intervals for repetitive inspections (e.g., 8,000 landings for sealant inspection).
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
All Airbus Model A300 airplanes.
AI-generated summary from the source AD text. Verify against the official source before acting.
Source: Official FAA Source ↗
Retrieved: Apr 4, 2026
Rights: U.S. Government Public Domain
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