AD 2006-09-05
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A310-200 and -300 | Airworthiness Directives; Airbus Model A310-200 and -300 Series Airplanes |
Unsafe Condition
Fatigue cracks in the lower rear spar internal angle and tee fitting, which could lead to rupture of these components and reduced structural integrity of the wings.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Perform repetitive rotating probe inspections for cracks in the rear spar internal angle and left/right sides of the tee fitting, and take related investigative/corrective actions if necessary. Modify holes in the internal angle and tee fitting by cold expansion.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 1,000 flight cycles or 1,600 flight hours after the effective date, whichever is first, for initial inspections. Repetitive inspections must be conducted at intervals not exceeding 9,100 flight cycles or 14,650 flight hours for A310-200 series, and 9,500 flight cycles or 15,000 flight hours for A310-300 series, depending on configuration.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
All Airbus Model A310-203, -204, -221, -222, -304, -322, -324, and -325 airplanes, regardless of modification status.
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
This site is not affiliated with or endorsed by the FAA. Always verify with official sources.