AD 2016-13-08
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A300 | Airworthiness Directives; Airbus Airplanes |
Unsafe Condition
Cracking of the lower tension bolt area at the rib one junction (both sides) of the lower wing, which could lead to crack initiation and reduced structural integrity of the airplane.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Conduct repetitive inspections for cracking of the fasteners and fitting around the fastener holes at the frame (FR) 40 lower wing location. Perform HFEC inspections and rototest inspections as specified. Repair any cracks or out-of-tolerance hole diameters using an approved method before further flight.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within the specified compliance time as outlined in the AD, which corresponds to the normal scheduled maintenance for most affected operators.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
All Airbus Model A300 series airplanes, including Model A300 B4-600, B4-600R, F4-600R series airplanes, and Model A300 C4-605R Variant F airplanes (collectively called Model A300-600 series airplanes).
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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