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:

$279,015.81

Total Fixed Cost

$212,692.91

Storage:

$840.00

Weather service:

$604.89

Insurance:

$28,448.83

Pilot training

$7,812.00

Miscellaneous expenses:

$1,734.46

Refurbishing and modernization:

$16,492.08

Depreciation:

$156,760.65

Total Variable Cost (51.6 Hrs)
Cost Per Hour = $1,285.33
Cost Per Mile = $4.15

$66,322.90

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:

$400.62

Misc: landing, parking, supplies,
catering, etc

$127.37

Engine (x2)

Manufacturer:

Pratt & Whitney

Model:

PT6A-52

Horsepower:

850 HP

Overhaul (HT):

3,600 Hrs