CESSNA P210 (turbine)

Aircraft
Name: 
P210 (turbine)
Manufacturer: 
Body: 
Narrow
Wing: 
Fixed Wing
WTC
L
Type Code: 
L1T
Engine: 
Turboprop
Engine Count: 
Single
Manufacturered 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: 
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

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