AD 2009-18-16
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A310-203 | Airworthiness Directives; Airbus Model A310-203, -204, -221, -222, -304, -322, -324, and -325 Airplanes |
| aircraft | Aviat | Various | Airworthiness Directives; Airbus Model A310-203, -204, -221, -222, -304, -322, -324, and -325 Airplanes |
Unsafe Condition
Fatigue cracking of the frame foot run-outs, which could lead to rupture of the frame foot and cracking in adjacent frames and skin, and which could result in reduced structural integrity of the fuselage.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect by rotating probe for cracking of holes H1 through H29 on frame (FR) 43 through 46 inclusive. Inspect holes H1 through H29 on FR 43 through 46 inclusive to determine the edge distance of the hole. Take corrective actions if necessary.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within the compliance times specified in Airbus SB A310-53-2124 Revision 02.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Airbus Model A310-203, -204, -221, -222, -304, -322, -324, and -325 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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