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1975 - 1981 CESSNA 310R II
Twin engine piston aircraft with retractable landing gear. The 310R II seats up to 5 passengers plus 1 pilot.
Market Stats
Performance specifications
Horsepower:
2 x 285 HP
Best Cruise Speed:
194 KIAS
Best Range (i):
661 NM
Fuel Burn @ 75%:
26.2 GPH
Stall Speed:
70 KIAS
Rate of climb:
1,662 FPM
Rate of climb (1 engine out):
370 FPM
Ceiling:
19,750 FT
Ceiling (1 engine out):
7,400 FT
Takeoff distance:
1,335 FT
Landing distance:
640 FT
Takeoff distance over 50ft obstacle:
1,700 FT
Landing distance over 50ft obstacle:
1,790 FT
Weights
Gross Weight:
5,500 LBS
Empty Weight:
3,603 LBS
Fuel capacity:
102 GAL
Ownership Costs 1975
Total Cost of Ownership:
$31,495.48
Total Fixed Cost
$12,248.13
Annual inspection cost:
$2,210.00
Storage:
$840.00
Weather service:
$604.89
Insurance:
$3,418.94
Refurbishing and modernization:
$783.98
Depreciation:
$4,390.31
-
Total Variable Cost (82.5 Hrs)
Cost Per Hour = $233.30
Cost Per Mile = $1.20
$19,247.35
-
Fuel cost per hour:
(26.2 gallons/hr @ $5.40/gal) $141.48
Oil cost per hour:
$5.30
Overhaul reserves:
$30.25
Hourly maintenance:
$33.15
Misc: landing, parking, supplies,
catering, etc$23.12
Engine (x2)
Manufacturer:
Cont Motor
Model:
IO-520-M
Horsepower:
285 HP
Overhaul (HT):
1,700 Hrs
Years before overhaul:
12
Also Consider
CESSNA 310Q (1970 - 1974)
Typical Price: $156,254.00
Total Cost of Ownership: $29,692.67
Best Cruise: 192 KIAS
(
2
)
Best Range: 680 NM
(
19
)
Fuelburn: 25.5 GPH
(
0.7
)