AD 63-08-05
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Sud Aviation | Caravelle SE 210 Model III | Airworthiness Directives; SUD AVIATION Models SE-210 Caravelle Mark III and VIR Aircraft |
| aircraft | Sud Aviation | Caravelle SE 210 Model VIR | Airworthiness Directives; SUD AVIATION Models SE-210 Caravelle Mark III and VIR Aircraft |
Unsafe Condition
Overtorquing and possible failure of frequently removed flight control system bolts and failure of flight controls.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Remove flight control system bolts with shank diameter less than 6 mm and replace with new bolts per Sud Service Bulletin No. 27-131, Revision 2. Modify flight control rod ends and bellcranks per Sud Service Bulletin No. 27-138, Revision 1.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 300 hours' time in service after the effective date of this AD on aircraft with 2,700 or more hours' time in service on the effective date, or before 3,000 hours' time in service on aircraft with less than 2,700 hours' time in service on the effective date.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
SUD AVIATION Models SE-210 Caravelle Mark III and VIR Aircraft.
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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