*****AIRCRAFT
“Cessna – 210 Centurion”*****
REFERENCE INFORMATION (by Aircraft performance
database)
*****Aircraft
Features*****
Wing position: High wing
Engine position: Nose mounted
Tail configuration: Regular tail, low set
Landing gear: Tricycle retractable
Wing Span: 11.2 m
Length: 8.6 m
Height: 3.0 m
Power plant: 210: 1 x 300 HP
Continental IO-520L piston engine with 3 blade propeller.
T210: 1 x 310 HP Continental TSIO-520R turbocharged piston engine with 3 blade propeller.
Accommodation: One pilot and up to 5 passengers.
Notes: 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. P210 (ICAO Designator: P210)
high performance pressurized type. Note: Similar to CESSNA 206 but with RG and
without wingstruts.
Alternative names:
AVIONES COLOMBIA 210,
Centurion, CESSNA
210,T210,(Turbo)Centurion
T210 Turbo Centurion, Turbo Centurion, CESSNA
210,Centurion
*****Total Flight
Simulator aircraft weight with full fuel*****
0000 lbs –
1.820 kg
VMO - Maximum Operating Speed 170 KIAS
MMO - Maximum Operating Speed Mach nd Mach
Turbulent Air Penetration Speed 000 KIAS/.00 Mach
VLO - Maximum Gear Operating Speed 000 KIAS
VLE - Maximum Landing Gear Extension Speed 000 KIAS/.00 Mach
*****Maximum
Flap Placard Speeds*****
Flaps degrees KIAS
0 000
1 0 0
2 0 0
3 full 0
gear down 0
(stalling 0)
*****Take-off*****
WTC: L
Distance: 400
mt
V2 (IAS): 70
kts
*****Climbing*****
-(to 5000 ft)
IAS: 100
kt
ROC: 500
ft/min
-(to FL150)
IAS: 140
kt
ROC: 500
ft/min
-(to FL240)
IAS: 140
kt
ROC: nd
ft/min
-(mach)
mach: nd
ROC: nd
ft/min
*****Cruise*****
TAS: 170
kt
MACh: nd
data
Ceiling: FL270
Range: 800
NM
*****Descent
*****
- (to FL240)
mach: nd
ROD: nd
ft/min
- (to FL100)
IAS: 170
kt
ROD: 500
ft/min
*****Approach*****
IAS: 170
kt
MCS: nd
kt
ROD: 500
ft/min
*****Landing*****
Vht (IAS): 75
kt
APC: A
Distance: 450 mt