AD 2016-16-06
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A300 B4-603 | Airworthiness Directives; Airbus Airplanes |
Unsafe Condition
Cracking of the door frame (FR) 73A between stringers 24 and 25, which could reduce structural integrity of the airplane.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect around the rivet heads of the seal retainer run-out holes at certain frames (FR 73A, FR 56A, and FR 57A) using high frequency eddy current (HFEC) inspections. Take corrective actions if cracks are detected.
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Compliance Time
Before further flight
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Affected Aircraft
Airbus Model A300 B4-603, B4-605R, and B4-622R airplanes; and Model A310-304, -324, and -325 airplanes in post-MOD 06924 configuration.
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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