AD 87-04-12
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A300 B2-1A | Airworthiness Directives; AIRBUS INDUSTRIE Model A300 B2 and B4 Series Airplanes |
| aircraft | Airbus | A300 B2-1C | Airworthiness Directives; AIRBUS INDUSTRIE Model A300 B2 and B4 Series Airplanes |
| aircraft | Airbus | A300 B2-203 | Airworthiness Directives; AIRBUS INDUSTRIE Model A300 B2 and B4 Series Airplanes |
| aircraft | Airbus | A300 B2K-3C | Airworthiness Directives; AIRBUS INDUSTRIE Model A300 B2 and B4 Series Airplanes |
| aircraft | Airbus | A300 B4-103 | Airworthiness Directives; AIRBUS INDUSTRIE Model A300 B2 and B4 Series Airplanes |
| aircraft | Airbus | A300 B4-203 | Airworthiness Directives; AIRBUS INDUSTRIE Model A300 B2 and B4 Series Airplanes |
| aircraft | Airbus | A300 B4-2C | Airworthiness Directives; AIRBUS INDUSTRIE Model A300 B2 and B4 Series Airplanes |
Unsafe Condition
Cracks in fuselage frame 47 may propagate, leading to structural failure.
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Required Actions
Inspect and repair cracks in fuselage frame 47 fastener holes per specified service bulletins. Reinspect at intervals not exceeding specified landing counts. Modifications per service bulletins may terminate inspection requirements.
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Compliance Time
Within the time period specified in each paragraph after the effective date (March 9, 1987), or prior to reaching the threshold number of landings indicated in each paragraph, whichever occurs later.
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Affected Aircraft
Airbus Model A300 B2 and B4 series airplanes, including specific models A300 B2-1A, B2-1C, B2-203, B2K-3C, B4-103, B4-203, B4-2C, with serial numbers as listed in applicable service bulletins.
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Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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