AD 2010-06-05
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A300 B4-2C | Airworthiness Directives; Airbus Model A300 B4-2C, B4-103, and B4-203 Airplanes; and Model A300 B4-601, B4-603, B4-620, B4-622, B4-605R, and B4-622R Airplanes |
| aircraft | Aviat | Various | Airworthiness Directives; Airbus Model A300 B4-2C, B4-103, and B4-203 Airplanes; and Model A300 B4-601, B4-603, B4-620, B4-622, B4-605R, and B4-622R Airplanes |
Unsafe Condition
Right Hand frame 40 forward fitting between stringer 32 and stringer 33 was found cracked. This condition, if not corrected, could result in a deterioration of the structural integrity of the frame.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect the Right Hand frame 40 forward fitting between stringer 32 and stringer 33 for cracks. Repair any cracks found to restore the original strength of the part.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 50 flight hours after the effective date of the AD.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Airbus Model A300 B4-2C, B4-103, B4-203, B4-601, B4-603, B4-605R, B4-620, B4-622, and B4-622R airplanes, all serial numbers, modified preventively in service in accordance with Airbus Service Bulletin A300-53-0297 or A300-57-6053 (Airbus Modification 10453).
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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