AD 2017-15-17
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A300 B4-600R | Airworthiness Directives; Airbus Airplanes |
Unsafe Condition
A crack could occur in the forward fitting lower radius of a certain frame after a certain number of flight cycles, potentially reducing the structural integrity of the fuselage.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect the lower area of a certain frame radius for cracking using a high frequency eddy current (HFEC) method. Take corrective action if cracking is detected. Extend the inspection area and perform an additional inspection for previously inspected airplanes.
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 B4-600R series airplanes, Model A300 C4-605R Variant F airplanes, and Model A300 F4-600R series airplanes.
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Source: Official FAA Source ↗
Retrieved: Apr 4, 2026
Rights: U.S. Government Public Domain
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