C10T
CESSNA P210 (turbine)
CESSNA P210 (turbine)
Aircraft
Name
P210 (turbine)
Manufacturer
Body
Narrow
Wing
Fixed Wing
WTC
L
Type Code
L1T
Engine
Turboprop
Engine Count
Single
Manufactured as
CESSNA P210 (turbine)
ADVANCED AIRCRAFT Spirit 750
ADVANCED AIRCRAFT Turbine P210
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 (metric)
11.20 m
Length (metric)
8.59 m
Height (metric)
2.95 m
Powerplant
1 x Rolls-Royce (Allison) 250-B17F/2 (450 shp).
Engine Model(s)
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
