1985 - 1986 CESSNA T210R Centurion Turbo
Single engine piston aircraft with retractable landing gear. The T210R Centurion Turbo seats up to 5 passengers plus 1 pilot.
Market Stats




Performance specifications
Horsepower:
1 x 325 HP
Best Cruise Speed:
207 KIAS
Best Range (i):
715 NM
Fuel Burn @ 75%:
17.8 GPH
Stall Speed:
55 KIAS
Rate of climb:
1,150 FPM
Ceiling:
29,000 FT
Takeoff distance:
1,270 FT
Landing distance:
825 FT
Takeoff distance over 50ft obstacle:
2,110 FT
Landing distance over 50ft obstacle:
1,600 FT
Weights
Gross Weight:
4,100 LBS
Empty Weight:
2,320 LBS
Maximum Payload:
1,618 LBS
Fuel capacity:
87 GAL
Ownership Costs 1985
Total Cost of Ownership:
Register For Free
Total Fixed Cost
Register For Free
Annual inspection cost:
Storage:
Weather service:
Insurance:
Refurbishing and modernization:
Depreciation:
-
Total Variable Cost (100 Hrs)
Cost Per Hour = $159.45
Cost Per Mile = $0.77
Register For Free
-
Fuel cost per hour:
(17.8 gallons/hr @ $5.40/gal) Oil cost per hour:
Overhaul reserves:
Hourly maintenance:
Misc: landing, parking, supplies,
catering, etc
Engine (x1)
Manufacturer:
Cont Motor
Model:
TSIO-520-CE
Horsepower:
325 HP
Overhaul (HT):
1,600 Hrs
Years before overhaul:
12
Also Consider
CESSNA T210M Turbo (1977 - 1978)
Typical Price: $233,134.00
Total Cost of Ownership: $28,847.64
Best Cruise: 197 KIAS
(
10
)
Best Range: 732 NM
(
17
)
Fuelburn: 17.0 GPH
(
0.8
)