AD 90-14-03
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Sud Aviation | Caravelle SE 210 Model III | Airworthiness Directives; AEROSPATIALE Caravelle SE 210 Model III and VIR Series Airplanes |
| aircraft | Sud Aviation | Caravelle SE 210 Model VIR | Airworthiness Directives; AEROSPATIALE Caravelle SE 210 Model III and VIR Series Airplanes |
Unsafe Condition
Fatigue cracks in the wing spar box could result in reduced structural integrity of the wings.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Perform an initial X-ray inspection on the wing lower surface stiffeners in the critical zone per SB 57-67 before 40,000 landings or within 1,000 landings after AD effective date, whichever is later. Repeat inspections at intervals not exceeding 2,500 landings if no cracks found. If cracks are found, evaluate with ultrasonic inspection, repair cracks prior to flight, and adjust inspection intervals based on crack length.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Prior to the accumulation of 40,000 landings or within 1,000 landings after the effective date of this AD, whichever occurs later.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
All Caravelle SE 210 Model III and VIR series airplanes, certificated in any category.
AI-generated summary from the source AD text. Verify against the official source before acting.
Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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