AD 94-09-15
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
Fatigue cracking in additional areas of the aft pressure bulkhead could lead to potential loss of cabin pressurization.
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Required Actions
Inspect the aft bulkhead in areas 1 and 2, then areas 3 and 4, and repair any detected cracks. Accomplish Airbus Modifications 2476/D1869 and 2476/D1842 to terminate inspection requirements.
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Compliance Time
Prior to the accumulation of specified flight cycles (12,000, 17,000, 32,000) or within specified timeframes (180 days, 1 year, 6 years) after effective dates, whichever occurs later.
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Affected Aircraft
Airbus Model A300 B2-1A, B2-1C, B2-203, B2K-3C, B4-103, B4-203, B4-2C series airplanes where Modifications 2476/D1842 and 2476/D1869 have not been done.
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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