P210
CESSNA P210 Pressurized Centurion
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 retractable
Manufactured as
RILEY Rocket P210
RILEY Super P210
CESSNA P210 Pressurized Centurion
CESSNA Pressurized Centurion
AVIONES COLOMBIA 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 (metric)
11.20 m
Length (metric)
8.59 m
Height (metric)
2.92 m
Powerplant
1 x 231 kW (310 hp) Continental TSIO-520-AF flat-six turbocharged engine, with three-blade constant-speed metal propeller
Engine Model(s)
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
