Cessna 210N

The Cessna 210N Centurion 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 1979–1984.

Cessna 210N Centurion is part of the retractable-gear Cessna 210 Centurion lineage certificated under FAA 3A21. The represented model uses the Continental IO-520-L rated at 300 hp, with a 3,800 lb maximum weight and 89 U.S. gallons usable fuel from a 90-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: 90 U.S. gallons. Standard usable fuel: 89 U.S. gallons. Earlier 210N serials use 89 gallons usable; later serials use 87 gallons usable.

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 ramp weight: 3,812 lb. Maximum takeoff weight: 3,800 lb. FAA 3A21 provides model-specific baggage/loading data; use the approved aircraft W&B record. The represented maximum weight is 3,800 lb with a 3,812 lb ramp limit. 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 210N Centurion calculator.