AD 2010-23-26
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A300 B2-1C | Airworthiness Directives; Airbus Model A300 B2-1C, B2K-3C, B2-203, B4-2C, B4-103, and B4-203 Airplanes; and Model A300 B4-601, B4-603, B4-620, B4-622, B4-605R, B4-622R, and F4-605R Airplanes |
| aircraft | Aviat | Various | Airworthiness Directives; Airbus Model A300 B2-1C, B2K-3C, B2-203, B4-2C, B4-103, and B4-203 Airplanes; and Model A300 B4-601, B4-603, B4-620, B4-622, B4-605R, B4-622R, and F4-605R Airplanes |
Unsafe Condition
Cracks on the MLG rib 5 RH and LH attachment fitting lower flanges, which could affect the structural integrity of the airplanes.
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Required Actions
Contact Airbus for repair instructions if necessary and perform the repair. Implement a new inspection program introduced in Revisions 3 of Airbus SB A300-57A0246 and Airbus SB A300-57A6101, including a new inspection technique for holes 47 and 54, and reduce inspection intervals from 700 Flight Cycles to 400 Flight Cycles until a revised terminating action is available.
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Compliance Time
Within 12 months of the effective date (January 5, 2011).
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Affected Aircraft
Airbus Model A300 B2-1C, B2K-3C, B2-203, B4-2C, B4-103, B4-203, B4-601, B4-603, B4-620, B4-622, B4-605R, B4-622R, and F4-605R airplanes.
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Source: Official FAA Source ↗
Retrieved: Apr 6, 2026
Rights: U.S. Government Public Domain
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