Aircraft › Cessna › 210 / T210 / P210 › P210R
The Cessna P210R is a model in the 210 / T210 / P210 family. It is described here as a Retractable-gear high-wing piston single.
Cessna P210R specifications
| Manufacturer | Cessna |
|---|---|
| Model | P210R |
| Production years | 1985–1986 |
| Aircraft type | Retractable-gear high-wing piston single |
| Landing gear | Retractable tricycle |
| Certification | FAA 3A21 |
Cessna P210R weights and capacities
| Maximum ramp weight | 4,116 lb |
|---|---|
| Maximum takeoff weight | 4,100 lb |
| Maximum landing weight | 3,900 lb |
FAA TCDS 3A21 directs use of the applicable weight-and-balance data for baggage/loading limits; no single universal baggage limit is represented.
Cessna P210R engine and configuration
| Engine | Continental · TSIO-520-CE · 325 hp · @ 2,700 rpm |
|---|
Fuel capacity and configuration
| standard fuel system | 90 gal total · 87 gal usable · standard fuel system |
|---|---|
| approved optional long-range fuel system | 120 gal total · 115 gal usable · approved optional long-range fuel system |
Baggage and loading applicability
| Baggage | FAA TCDS 3A21 directs use of the applicable weight-and-balance data for baggage/loading limits; no single universal baggage limit is represented. |
|---|
Cessna P210R history and development
The cataloged production period is 1985–1986.
Cessna P210R is a member of the Cessna 210 / T210 / P210 Centurion family covered by FAA TCDS 3A21. This batch includes the late 210R, turbocharged T210F through T210R, and pressurized P210N/P210R branches. The family contains substantial engine, turbocharging, pressurization, gross-weight and fuel-system changes, so unresolved technical figures are not transferred between suffixes.
Cessna P210R fuel capacity
exact model-specific fuel capacity / usable fuel has not yet been verified from the applicable certification record, approved flight manual, or manufacturer data. Do not infer it from a neighboring Cessna/Reims-Cessna model or suffix.
Cessna P210R model applicability and configuration
Verify exact model designation, serial number, engine, fuel installation and approved configuration against the applicable certification record and individual aircraft documentation.
Cessna P210R weight and balance
Use the exact model/serial-number loading data and the individual aircraft's approved weight-and-balance record. No baggage limit is inferred from a related model. The exact model-specific maximum takeoff weight / gross weight remains unverified until the applicable approval section is verified. Operational loading must use the aircraft-specific empty weight, CG, station arms and limitations. Use the approved aircraft-specific documentation and current weight-and-balance record for operational calculations. WBcalc does not currently provide a model-specific Cessna P210R calculator.
Reference sources
FAA: FAA Type Certificate Data Sheet 3A21
Related 210 / T210 / P210 models
- Cessna 210 - 1960
- Cessna 210A - 1961
- Cessna 210B - 1962
- Cessna 210C - 1963
- Cessna 210D - 1964
- 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