AD 76-14-07 R2
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Cessna Aircraft Company | 210 | Airworthiness Directives; CESSNA Models 210 thru 210J and Models T210F thru T210J Airplanes |
| aircraft | Cessna Aircraft Company | 210A | Airworthiness Directives; CESSNA Models 210 thru 210J and Models T210F thru T210J Airplanes |
| aircraft | Cessna Aircraft Company | 210B | Airworthiness Directives; CESSNA Models 210 thru 210J and Models T210F thru T210J Airplanes |
| aircraft | Cessna Aircraft Company | 210C | Airworthiness Directives; CESSNA Models 210 thru 210J and Models T210F thru T210J Airplanes |
| aircraft | Cessna Aircraft Company | 210D | Airworthiness Directives; CESSNA Models 210 thru 210J and Models T210F thru T210J Airplanes |
| aircraft | Cessna Aircraft Company | 210E | Airworthiness Directives; CESSNA Models 210 thru 210J and Models T210F thru T210J Airplanes |
| aircraft | Cessna Aircraft Company | 210F | Airworthiness Directives; CESSNA Models 210 thru 210J and Models T210F thru T210J Airplanes |
| aircraft | Cessna Aircraft Company | 210G | Airworthiness Directives; CESSNA Models 210 thru 210J and Models T210F thru T210J Airplanes |
| aircraft | Cessna Aircraft Company | 210H | Airworthiness Directives; CESSNA Models 210 thru 210J and Models T210F thru T210J Airplanes |
| aircraft | Cessna Aircraft Company | 210J | Airworthiness Directives; CESSNA Models 210 thru 210J and Models T210F thru T210J Airplanes |
Unsafe Condition
Cracks in Part Numbers 1241004-1, 1241004-2, 1241423-1, and 1241423-2 landing gear saddles could lead to main landing gear extension failures.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect landing gear saddles using dye penetrant procedures; replace cracked saddles before further flight. Replace specific part numbers with new components within 100 hours time in service after August 16, 1976, or prior to April 1, 1977, and at each 1,000 hours thereafter. Annual inspections are required for certain models after specific time-in-service thresholds.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Compliance required as indicated, with specific deadlines including within 25 hours time in service after the effective date, 100 hours time in service after August 16, 1976, or prior to April 1, 1977, and subsequent intervals based on time-in-service.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Cessna Models 210 thru 210J (Serial Numbers 57001 thru 57575, 21057576 thru 21059199) and Models T210F thru T210J (Serial Numbers T210-0001 thru T210-0454).
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.