C210
CESSNA 210 Centurion
CESSNA 210 Centurion
Aircraft
Name
210 Centurion
Manufacturer
Body
Narrow
Wing
Fixed Wing
Position
High wing
Tail
Regular tail, low set
WTC
L
APC
A
Type Code
L1P
Engine
Piston
Engine Count
Single
Position
Nose mounted
Landing gear
Tricycle retractable
Manufactured as
CESSNA 210
CESSNA Centurion
CESSNA Turbo Centurion
CESSNA T210 Turbo Centurion
CESSNA 210 Centurion
AVIONES COLOMBIA 210
C210
High performance light aircraft. In service since 1960. Exists in several versions with different engines. Has been constantly updated but production of the basic version ceased in 1985. The P210 is the high performance pressurized type. Note: Similar to CESSNA 206 but with retractable gear and without wingstruts.
Technical Data
Wing span (metric)
11.20 m
Length (metric)
8.60 m
Height (metric)
3.00 m
Powerplant
210: 1 x 300 HP Continental IO-520L piston engine with 3 blade propeller.
Engine Model(s)
Continental O-520
Indicative Performance Data
Take-Off
V2
70 kts
Distance
400 m
MTOW
1820 kg
Initial Climb (to 5000 ft)
IAS
100 kts
ROC
500 ft/min
Initial Climb (to FL150)
IAS
140 kts
ROC
-500
Initial Climb (to FL240)
IAS
140 kts
ROC
n/a
MACH Climb
MACH
n/a
ROC
n/a
Cruise
TAS
170 kts
MACH
n/a
Ceiling
270
Range
800 NM
Initial Descent (to FL240)
MACH
n/a
ROD
n/a
Descent (to FL100)
IAS
170 kts
ROD
500 ft/min
Descent (FL100 & below)
IAS
n/a
MCS
n/a
ROD
n/a
Approach
Vapp (IAS)
75 kts
Distance
450 m
