AD 2006-02-06
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A310-203 | Airworthiness Directives; Airbus Model A310-203, -204, and -222 Airplanes, and Model A310-300 Series Airplanes |
Unsafe Condition
Fatigue cracking of the frame foot run-outs from fuselage frames (FR) 43 through FR 46, which could lead to rupture of the frame foot and cracking in adjacent frames and fuselage skin, resulting in reduced structural integrity of the fuselage.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Perform a one-time rototest inspection for cracking of the frame foot and adjacent frames and skin in the area surrounding the frame foot run-outs from fuselage frames FR 43 through FR 46. Repair any cracking before further flight. Modify fastener holes located between FR 43 and FR 46 on the center box and upper fuselage bent sections.
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Compliance Time
Within 3,000 flight cycles after the effective date of this AD or before the accumulation of the total flight-cycle or flight-hour threshold specified in the Accomplishment Timescale table of Airbus Service Bulletin A310-53-2124.
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Affected Aircraft
Airbus Model A310-203, -204, and -222 airplanes, and Model A310-304, -322, -324, and -325 airplanes; certificated in any category; except those airplanes on which Airbus Modification 13023 has been accomplished in production.
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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