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1965 - 1968 DASSAULT FALCON 20C-5 (AR)
Twin engine turbofan aircraft. The FALCON 20C-5 (AR) seats up to 9 passengers plus 2 pilot(s).
Market Stats
Performance specifications
Thrust:
2 x 4,500 N
Best Cruise Speed:
455 KIAS
Best Range (i):
2,260 NM
Fuel Burn:
249.0 GPH
Rate of climb:
3,500 FPM
Rate of climb (1 engine out):
405 FPM
Ceiling:
42,000 FT
Takeoff distance:
6,650 FT
Landing distance:
3,233 FT
Weights
Gross Weight:
30,325 LBS
Empty Weight:
16,965 LBS
Maximum Payload:
5,100 LBS
Fuel capacity:
1,237 GAL
Ownership Costs 1967
Total Cost of Ownership:
$897,320.17
Total Fixed Cost
$256,317.04
Storage:
$20,821.99
Weather service:
$604.89
Insurance:
$5,739.57
Pilot salary, taxes and benefits
$133,076.16
Pilot training
$45,225.00
Miscellaneous expenses:
$9,451.51
Refurbishing and modernization:
$6,957.05
Depreciation:
$34,440.87
-
Total Variable Cost (241.8 Hrs)
Cost Per Hour = $2,650.96
Cost Per Mile = $5.83
$641,003.13
-
Fuel cost per hour:
(249.0 gallons/hr @ $4.90/gal) $1,220.20
Oil cost per hour:
$0.00
Overhaul reserves:
$635.50
Hourly maintenance:
$532.56
Misc: landing, parking, supplies,
catering, etc$262.71
Engine (x2)
Manufacturer:
Honeywell Engines
Model:
TFE 731-5AR
Thrust:
4,500 N
Overhaul (HT):
4,200 Hrs
Also Consider
DASSAULT Falcon 20F-5 (1983 - 1988)
Best Cruise: 410 KIAS
(
45
)
Best Range: 2257 NM
(
3
)
Fuelburn: 248.5 GPH
(
0.5
)