Twin engine turboprop aircraft with retractable landing gear. The KING AIR 250 seats up to 10 passengers plus 1 pilot.

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Performance specifications

Horsepower:

2 x 850 HP

Best Cruise Speed:

310 KIAS

Best Range (i):

1,582 NM

Fuel Burn:

83.6 GPH

Stall Speed:

75 KIAS

Rate of climb:

2,437 FPM

Rate of climb (1 engine out):

682 FPM

Ceiling:

35,000 FT

Ceiling (1 engine out):

26,000 FT

Takeoff distance:

2,111 FT

Landing distance:

2,845 FT

Takeoff distance over 50ft obstacle:

2,111 FT

Landing distance over 50ft obstacle:

2,845 FT

Weights

Gross Weight:

12,500 LBS

Empty Weight:

8,830 LBS

Maximum Payload:

2,220 LBS

Fuel capacity:

544 GAL

Ownership Costs 2011

Total Cost of Ownership:

$328,992.45

Total Fixed Cost

$203,106.09

Storage:

$840.00

Weather service:

$604.89

Insurance:

$26,679.95

Pilot training

$7,812.00

Miscellaneous expenses:

$1,653.09

Refurbishing and modernization:

$15,466.64

Depreciation:

$150,049.51

Total Variable Cost (100 Hrs)
Cost Per Hour = $1,258.86
Cost Per Mile = $4.06

$125,886.36

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

$451.33

Oil cost per hour:

$0.00

Overhaul reserves:

$306.00

Hourly maintenance:

$376.78

Misc: landing, parking, supplies,
catering, etc

$124.75

Engine (x2)

Manufacturer:

Pratt & Whitney

Model:

PT6A-52

Horsepower:

850 HP

Overhaul (HT):

3,600 Hrs