AD 90-10-01
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Sud Aviation | Caravelle SE 210 Model I | Airworthiness Directives; AEROSPATIALE (FORMERLY SUD AVIATION/SUD-SERVICE): Caravelle Model SE 210 Series Airplanes |
| aircraft | Sud Aviation | Caravelle SE 210 Model III | Airworthiness Directives; AEROSPATIALE (FORMERLY SUD AVIATION/SUD-SERVICE): Caravelle Model SE 210 Series Airplanes |
| aircraft | Sud Aviation | Caravelle SE 210 Model VIR | Airworthiness Directives; AEROSPATIALE (FORMERLY SUD AVIATION/SUD-SERVICE): Caravelle Model SE 210 Series Airplanes |
Unsafe Condition
Fatigue cracks in the wing-to-fuselage junction and fuselage lower section components, and sheared bolts or rivets in the wing-to-fuselage junction fittings at Frames 31 and 35, and in Fittings 210.12.52.382/383 and 210.22.53.012.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Perform inspections (visual, eddy current, magnetic particle, or dye penetrant) per Aerospatiale Service Bulletins 53-51 and 53-52. Replace or repair cracked components or sheared hardware prior to further flight. Repeat inspections at intervals not exceeding specified landing counts.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Prior to the accumulation of 29,000 landings, or within 2,000 landings after the effective date (June 1, 1990), whichever occurs later.
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Affected Aircraft
Aerospatiale Caravelle Model SE 210 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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