CESSNA P210 Pressurized Centurion

Aircraft
Name: 
P210 Pressurized Centurion
Manufacturer: 
Body: 
Narrow
Wing: 
Fixed Wing
Position: 
High wing
Tail: 
Regular tail, low set
WTC
L
Type Code: 
L1P
Engine: 
Piston
Engine Count: 
Single
Position: 
Nose mounted
Landing gear: 
Tricycle fixed
Manufacturered as
CESSNA P210 Pressurized Centurion
CESSNA Pressurized Centurion
AVIONES COLOMBIA P210
RILEY Rocket P210
RILEY Super P210

P210

Pressurized CESSNA 210 Centurion. Note: Pressurized version has distinctive small windows. The P210 (turbine) is a modified version with a turbine engine.

Technical Data
Wing span: 
11.20 m
Length: 
8.59 m
Height: 
2.92 m
Powerplant: 

Variants:

Engine Model: 
Continental O-520
Indicative Performance Data
Take-Off
V2: 
n/a
Distance: 
396 m
MTOW: 
1814 kg
Initial Climb (to 5000 ft)
IAS: 
n/a
ROC: 
900 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: 
200 kts
MACH: 
n/a
Ceiling: 
230
Range: 
925 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: 
233 m

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