AD 2014-20-18
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A300 B4-605R and B4-622R | Airworthiness Directives; Airbus Airplanes |
Unsafe Condition
Fatigue cracking of the forward fitting of fuselage frame FR47 could result in reduced structural integrity of the frame.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Perform new repetitive ultrasonic inspections for cracks of the center wing box lower panel and repair if necessary. Remove certain airplanes from applicability.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Before further flight
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Affected Aircraft
Airbus Model A300 B4-605R and B4-622R; Model A300 F4-605R; Model A300 C4-605R Variant F airplanes.
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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