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
Cite This Page
SKYbrary Aviation Safety. (March 8, 2021). C10T.
Retrieved June 4, 2026
from https://skybrary.aero/aircraft/c10t
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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
