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1967 - 1968 CESSNA 411A
Twin engine piston aircraft with retractable landing gear. The 411A seats up to 7 passengers plus 1 pilot.
Market Stats
Performance specifications
Horsepower:
2 x 340 HP
Best Cruise Speed:
214 KIAS
Best Range (i):
908 NM
Fuel Burn @ 75%:
43.0 GPH
Stall Speed:
72 KIAS
Rate of climb:
1,900 FPM
Rate of climb (1 engine out):
320 FPM
Ceiling:
26,000 FT
Ceiling (1 engine out):
13,000 FT
Takeoff distance:
1,560 FT
Landing distance:
1,240 FT
Takeoff distance over 50ft obstacle:
2,010 FT
Landing distance over 50ft obstacle:
1,851 FT
Weights
Gross Weight:
6,500 LBS
Empty Weight:
3,865 LBS
Fuel capacity:
175 GAL
Ownership Costs 1967
Total Cost of Ownership:
$42,871.99
Total Fixed Cost
$15,033.92
Annual inspection cost:
$3,250.00
Storage:
$840.00
Weather service:
$604.89
Insurance:
$4,259.00
Refurbishing and modernization:
$966.86
Depreciation:
$5,113.18
-
Total Variable Cost (74.8 Hrs)
Cost Per Hour = $372.17
Cost Per Mile = $1.74
$27,838.07
-
Fuel cost per hour:
(43.0 gallons/hr @ $5.40/gal) $232.20
Oil cost per hour:
$5.90
Overhaul reserves:
$48.44
Hourly maintenance:
$48.75
Misc: landing, parking, supplies,
catering, etc$36.88
Engine (x2)
Manufacturer:
Cont Motor
Model:
GTSIO-520-C
Horsepower:
340 HP
Overhaul (HT):
1,600 Hrs
Years before overhaul:
12
Also Consider
CESSNA 402A (1969 - 1969)
Best Cruise: 209 KIAS
(
5
)
Best Range: 833 NM
(
75
)
Fuelburn: 32.0 GPH
(
11.0
)