AD 64-27-03
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Sud Aviation | Caravelle SE 210 Model VIR | Airworthiness Directives; SUD AVIATION Model SE 210 Caravelle VIR Aircraft |
Unsafe Condition
Fatigue failure of the main landing gear steel axle beams due to cracks around threaded holes.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Visually inspect main landing gear steel axle beams (P/N 269028B and 269029B) for cracks around threaded holes as specified in Hispano Suiza Aeroservice Bulletin No. 91 Section 1, No. 34. Perform inspections with magnifying glass and fluorescent magnetic particle inspection as required. Rework holes per specified bulletin and replace cracked parts before flight.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 430 hours' time in service after January 1, 1965, and at intervals not exceeding 430 hours' time in service. Additional inspections required at 5,530 hours' total time in service or within 430 hours' total time in service based on existing hours. Rework required by 8,000 and 12,000 hours' total time in service.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
SUD AVIATION Model SE 210 Caravelle VIR Aircraft with main landing gear steel axle beams P/N 269028B and 269029B.
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
This site is not affiliated with or endorsed by the FAA. Always verify with official sources.