AD 88-04-08
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Sud Aviation | Caravelle SE 210 Model I | Airworthiness Directives; SUD AVIATION Model Caravelle SE210 Series Airplanes |
| aircraft | Sud Aviation | Caravelle SE 210 Model III | Airworthiness Directives; SUD AVIATION Model Caravelle SE210 Series Airplanes |
| aircraft | Sud Aviation | Caravelle SE 210 Model VIR | Airworthiness Directives; SUD AVIATION Model Caravelle SE210 Series Airplanes |
Unsafe Condition
Breakage of main landing gear manual uplock release mechanism screwjack shaft.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Perform inspections of the square end fitting and screwjack shafts as described in Sud Service Bulletin No. 32-121. Repeat inspections at intervals not exceeding 5,000 landings or 2 years (if Sud SB 32-96 not done) or 15,000 landings or 6 years (if Sud SB 32-96 done). Replace affected parts if damage, cracks, or more than two pin holes are found.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Prior to the accumulation of 2,500 landings or 12 months, whichever occurs first after the effective date of this AD.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Sud Aviation Model Caravelle SE210 series airplanes listed in Sud Service Bulletin No. 32-121, dated September 9, 1982.
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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