Twin engine turboprop aircraft with retractable landing gear. The KING AIR A200 seats up to 12 passengers plus 1 pilot.

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Performance specifications

Horsepower:

2 x 850 HP

Best Cruise Speed:

279 KIAS

Best Range (i):

2,185 NM

Fuel Burn:

132.8 GPH

Stall Speed:

74 KIAS

Rate of climb:

2,450 FPM

Rate of climb (1 engine out):

738 FPM

Ceiling:

31,000 FT

Takeoff distance:

2,579 FT

Takeoff distance over 50ft obstacle:

2,579 FT

Landing distance over 50ft obstacle:

2,074 FT

Weights

Gross Weight:

12,500 LBS

Empty Weight:

7,437 LBS

Maximum Payload:

4,250 LBS

Fuel capacity:

544 GAL

Ownership Costs 1975

Total Cost of Ownership:

$106,979.42

Total Fixed Cost

$33,983.08

Storage:

$840.00

Weather service:

$604.89

Insurance:

$4,987.67

Pilot training

$7,812.00

Miscellaneous expenses:

$655.25

Refurbishing and modernization:

$2,891.40

Depreciation:

$16,191.86

Total Variable Cost (57.3 Hrs)
Cost Per Hour = $1,273.93
Cost Per Mile = $4.56

$72,996.35

Fuel cost per hour:
(132.8 gallons/hr @ $5.40/gal)

$717.28

Oil cost per hour:

$0.00

Overhaul reserves:

$346.00

Hourly maintenance:

$84.41

Misc: landing, parking, supplies,
catering, etc

$126.25

Engine (x2)

Manufacturer:

Pratt & Whitney

Model:

PT6A-41

Horsepower:

850 HP

Overhaul (HT):

3,000 Hrs