Aircraft › Cessna › 210 / T210 / P210 › 210D
The Cessna 210D 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.
Cessna 210D specifications
| Manufacturer | Cessna |
|---|---|
| Model | 210D |
| Production years | 1964 |
| Aircraft type | Retractable-gear high-wing piston single |
| Seats | 4 |
| Landing gear | Retractable tricycle |
| Certification | FAA 3A21 |
Cessna 210D weights and capacities
| Maximum takeoff weight | 3,100 lb |
|---|---|
| Standard fuel capacity | 65 gal total / 63.4 gal usable |
FAA 3A21 provides model-specific baggage/loading data; use the approved aircraft W&B record.
Cessna 210D engine and configuration
| Engine | Continental · IO-470-S · 260 hp |
|---|
Baggage and loading applicability
| Baggage | FAA 3A21 provides model-specific baggage/loading data; use the approved aircraft W&B record. |
|---|
Cessna 210D history and development
The cataloged production period is 1964.
Cessna 210D is part of the retractable-gear Cessna 210 Centurion lineage certificated under FAA 3A21. The represented model uses the Continental IO-470-S rated at 260 hp, with a 3,100 lb maximum weight and 63.4 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.
Cessna 210D fuel capacity
Standard total fuel: 65 U.S. gallons. Standard usable fuel: 63.4 U.S. gallons.
Cessna 210D model applicability and configuration
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.
Cessna 210D weight and balance
Maximum takeoff weight: 3,100 lb. FAA 3A21 provides model-specific baggage/loading data; use the approved aircraft W&B record. The represented maximum weight is 3,100 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 210D calculator.
Cessna 210D frequently asked questions
What engine does the Cessna 210D use?
The engine listed for this model is Continental IO-470-S.
What is the maximum takeoff weight of the Cessna 210D?
The represented maximum takeoff weight is 3,100 lb.
How much usable fuel does the Cessna 210D carry?
The represented standard usable fuel capacity is 63.4 U.S. gallons.
Reference sources
FAA: Type Certificate Data Sheet 3A21, Revision 50 - Cessna 210 series
Related 210 / T210 / P210 models
- Cessna 210 - 1960
- Cessna 210A - 1961
- Cessna 210B - 1962
- Cessna 210C - 1963
- Cessna 210E - 1965
- Cessna 210F - 1966
- Cessna 210G - 1967
- Cessna 210H - 1968
- Cessna 210J - 1969
- Cessna 210K - 1970–1971
- Cessna 210L - 1972–1976
- Cessna 210M - 1977–1978
- Cessna 210N - 1979–1984
- Cessna 210R - 1985–1986
- Cessna T210F - 1966
- Cessna T210G - 1967
- Cessna T210H - 1968
- Cessna T210J - 1969
- Cessna T210K - 1970–1971
- Cessna T210L - 1972–1976
- Cessna T210M - 1977–1978
- Cessna T210N - 1979–1984
- Cessna T210R - 1985–1986
- Cessna P210N - 1978–1983
- Cessna P210R - 1985–1986