AD 2000-26-14
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A310 | Airworthiness Directives; Airbus Model A310 Series Airplanes |
Unsafe Condition
Cracks propagating from the fastener holes that attach the left- and right-hand pick-up angles at frame 40 to the wing lower skin and fuselage panel, leading to reduced structural integrity due to fatigue damage.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Perform a detailed visual inspection to detect cracks propagating from the fastener holes at frame 40. If cracking is found, perform corrective actions including repair (drilling and reaming a crack stop hole, Rototest inspection, and repetitive detailed visual inspections) or immediate replacement of the cracked pick-up angle. Repeat inspections at specified intervals based on model and flight history.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Initial inspection due within 700 flight cycles or 1,200 flight hours after the effective date, or prior to specified flight cycle or hour thresholds, depending on model and flight history.
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Affected Aircraft
All Airbus Model A310 series airplanes, regardless of modifications, alterations, or repairs.
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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