Aircraft › Cessna › 210 / T210 / P210 › T210N
The Cessna T210N is a model in the 210 / T210 / P210 family. It is described here as a Retractable-gear high-wing piston single.
Cessna T210N specifications
| Manufacturer | Cessna |
|---|---|
| Model | T210N |
| Production years | 1979–1984 |
| Aircraft type | Retractable-gear high-wing piston single |
| Landing gear | Retractable tricycle |
| Certification | FAA 3A21 |
Cessna T210N weights and capacities
| Maximum ramp weight | 4,016 lb |
|---|---|
| Maximum takeoff weight | 4,000 lb |
| Maximum landing weight | 3,800 lb |
Maximum baggage is controlled by the applicable approved weight-and-balance data / loading instructions for the individual aircraft.
Cessna T210N engine and configuration
| Engine | Continental · TSIO-520-R · 310 hp · @ 2,700 rpm · 310 hp takeoff rating for 5 minutes; 285 hp rating for other operations. |
|---|
Fuel capacity and configuration
| S/N 21062955 through 21064535 | 90 gal total · 89 gal usable · S/N 21062955 through 21064535 |
|---|---|
| S/N 21064536 and up | 90 gal total · 87 gal usable · S/N 21064536 and up |
Baggage and loading applicability
| Baggage | Maximum baggage is controlled by the applicable approved weight-and-balance data / loading instructions for the individual aircraft. |
|---|
Cessna T210N history and development
The cataloged production period is 1979–1984.
Cessna T210N 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 T210N 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 T210N 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 T210N 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 T210N calculator.
Reference sources
FAA: FAA TCDS 3A21 - Model T210N
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 T210R - 1985–1986
- Cessna P210N - 1978–1983
- Cessna P210R - 1985–1986