AD 88-06-05
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Sud Aviation | Caravelle SE 210 Model I | Airworthiness Directives; SUD AVIATION Caravelle Series Airplanes |
| aircraft | Sud Aviation | Caravelle SE 210 Model III | Airworthiness Directives; SUD AVIATION Caravelle Series Airplanes |
| aircraft | Sud Aviation | Caravelle SE 210 Model VIR | Airworthiness Directives; SUD AVIATION Caravelle Series Airplanes |
Unsafe Condition
Failure of the wing due to cracking adjacent to wing rib No. 31.
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Required Actions
Perform visual and nondestructive testing inspections (NDI) or radiographic inspections for cracking adjacent to wing rib No. 31, depending on the presence of external doublers. Repeat inspections at intervals specified in Service Bulletin 57-56, Revision 2, and repair any detected cracks prior to further flight.
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Compliance Time
Within 100 landings after the effective date of this AD or prior to the accumulation of the number of landings specified in the schedule (30,000, 20,000, or 10,000 landings based on maximum take-off weight), whichever occurs later.
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Affected Aircraft
Sud Aviation Caravelle SE 210 Model I, III, and VIR airplanes listed in Sud Aviation Caravelle Service Bulletin No. 57-56, Revision 2, dated February 28, 1985.
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Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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