AD 2006-19-02
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A300 B4-600 | Airworthiness Directives; Airbus Model A300 B4-600, B4-600R, and F4-600R Series Airplanes, and Model A300 C4-605R Variant F Airplanes (Collectively Called A300-600 Series Airplanes) |
Unsafe Condition
Fatigue cracking of the outer skin of the fuselage at certain frames, which could result in reduced structural integrity, and consequent rapid decompression of the airplane.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Conduct a one-time eddy current inspection for cracking of the fuselage outer skin at frames 28A and 30A above stringer 30, and repair if necessary. This inspection must be done before the reinforcement specified in the AD.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 12 months after August 4, 1997, or prior to the accumulation of 14,100 total flight cycles, whichever occurs later.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Airbus Model A300 B4-601, B4-603, B4-620, B4-622, B4-605R, B4-622R, F4-605R, F4-622R, and C4-605R Variant F airplanes, certificated in any category, except those on which Airbus Modification 8683 has been done.
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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