CESSNA P210 (turbine)
CESSNA P210 (turbine)
C10T
P210 The Cessna 210 Centurion is a six-seat, high-performance, retractable-gear single-engined general aviation aircraft which was first flown in January 1957 and produced by Cessna until 1985.
Technical Data
Wing span:
11.20 m
Length:
8.59 m
Height:
2.95 m
Powerplant:
1 x Rolls-Royce (Allison) 250-B17F/2 (450 shp).
Engine Model:
Allison 250
Indicative Performance Data
Take-Off
V2:
n/a
Distance:
n/a
MTOW:
1814 kg
Initial Climb (to 5000 ft)
IAS:
n/a
ROC:
930 ft/min
Initial Climb (to FL150)
IAS:
n/a
ROC:
n/a
Initial Climb (to FL240)
IAS:
n/a
ROC:
n/a
MACH Climb
MACH:
n/a
ROC:
n/a
Cruise
TAS:
193 kts
MACH:
n/a
Ceiling:
270
Range:
900 NM
Initial Descent (to FL240)
MACH:
n/a
ROD:
n/a
Descent (to FL100)
IAS:
n/a
ROD:
n/a
Descent (FL100 & below)
IAS:
n/a
MCS:
n/a
ROD:
n/a
Approach
Vapp (IAS):
n/a
Distance:
n/a
