AD 87-24-05
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A300 B2-1A | Airworthiness Directives; AIRBUS INDUSTRIE Model A300 Series Airplanes |
| aircraft | Airbus | A300 B2-1C | Airworthiness Directives; AIRBUS INDUSTRIE Model A300 Series Airplanes |
| aircraft | Airbus | A300 B2-203 | Airworthiness Directives; AIRBUS INDUSTRIE Model A300 Series Airplanes |
| aircraft | Airbus | A300 B2K-3C | Airworthiness Directives; AIRBUS INDUSTRIE Model A300 Series Airplanes |
| aircraft | Airbus | A300 B4-103 | Airworthiness Directives; AIRBUS INDUSTRIE Model A300 Series Airplanes |
| aircraft | Airbus | A300 B4-203 | Airworthiness Directives; AIRBUS INDUSTRIE Model A300 Series Airplanes |
| aircraft | Airbus | A300 B4-2C | Airworthiness Directives; AIRBUS INDUSTRIE Model A300 Series Airplanes |
Unsafe Condition
Corrosion in the lower rim area of the rear pressure bulkhead could lead to structural failure.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Perform a visual inspection for corrosion in the lower rim area of the rear pressure bulkhead and repair if necessary, following Airbus Industrie Service Bulletin A300-53-213.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Prior to further flight, within specified timeframes based on the airplane's years since first flight in revenue service: 6 months after reaching 4.5 years, next 6 months if between 4.5 and 6 years, or next 3 months if 6 years or more since first flight.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
AIRBUS INDUSTRIE Model A300 B2-1A, B2-1C, B2-203, B2K-3C, B4-103, B4-203, B4-2C series airplanes 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 8, 2026
Rights: U.S. Government Public Domain
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