AD 2011-17-05
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A300 B2-1C | Airworthiness Directives; Airbus Model A300 B2-1C, A300 B2-203, A300 B2K-3C, A300-B4-103, A300 B4-203, and A300 B4-2C Airplanes |
| aircraft | Aviat | Various | Airworthiness Directives; Airbus Model A300 B2-1C, A300 B2-203, A300 B2K-3C, A300-B4-103, A300 B4-203, and A300 B4-2C Airplanes |
Unsafe Condition
Cracks in sections 13 to 18 of the fuselage between rivets of longitudinal lap joints between frames 18 and 80, which could affect the structural integrity of the fuselage if not corrected.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Perform repetitive detailed inspections for disbonding and cracking of the fuselage inner doubler; conduct eddy current and ultrasonic inspections of the fuselage longitudinal lap joints for cracking; and repair any cracking or disbonding, or contact Airbus for repair instructions and perform the repair as necessary.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 2,000 flight cycles after the effective date of this AD, or prior to the accumulation of 24,000 total flight cycles, whichever occurs first.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Airbus Model A300 B2-1C, A300 B2-203, A300 B2K-3C, A300-B4-103, A300 B4-203, and A300 B4-2C airplanes; certificated in any category; serial numbers 0003 through 0156 inclusive.
AI-generated summary from the source AD text. Verify against the official source before acting.
Source: Official FAA Source ↗
Retrieved: Apr 6, 2026
Rights: U.S. Government Public Domain
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