Cessna 210A

The Cessna 210A is a model in the 210 / T210 / P210 family. It is described here as a Retractable-gear high-wing piston single. FAA type-certificate reference: 3A21.

The cataloged production period is 1961.

Cessna 210A is part of the retractable-gear Cessna 210 Centurion lineage certificated under FAA 3A21. The represented model uses the Continental IO-470-E rated at 260 hp, with a 2,900 lb maximum weight and 55 U.S. gallons usable fuel from a 65-gallon system. The 210 evolved substantially through the 1960s and 1970s, including changes in seating, engine, gross weight, wing fuel system and landing-gear structure, so each suffix is kept as its own model reference.

Standard total fuel: 65 U.S. gallons. Standard usable fuel: 55 U.S. gallons.

Apply these figures only to the exact 210 model/serial-number branch covered by FAA 3A21. Fuel capacity, engine dash number, seats and approved modifications can vary. Verify the data plate, POH/AFM, equipment list and current weight-and-balance report for the individual aircraft.

Maximum takeoff weight: 2,900 lb. FAA 3A21 provides model-specific baggage/loading data; use the approved aircraft W&B record. The represented maximum weight is 2,900 lb. Operational loading must use the aircraft-specific empty weight, CG and baggage station limits. Use the approved aircraft-specific documentation and current weight-and-balance record for operational calculations. WBcalc does not currently provide a model-specific Cessna 210A calculator.