Twin engine turboprop aircraft with retractable landing gear. The KING AIR C90GTi seats up to 7 passengers plus 1 pilot.

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Performance specifications

Horsepower:

2 x 550 HP

Best Cruise Speed:

272 KIAS

Best Range (i):

1,100 NM

Fuel Burn:

91.0 GPH

Stall Speed:

78 KIAS

Rate of climb:

1,953 FPM

Rate of climb (1 engine out):

474 FPM

Ceiling:

30,000 FT

Ceiling (1 engine out):

19,170 FT

Takeoff distance:

2,392 FT

Landing distance:

2,355 FT

Takeoff distance over 50ft obstacle:

2,392 FT

Landing distance over 50ft obstacle:

2,355 FT

Weights

Gross Weight:

10,100 LBS

Empty Weight:

6,950 LBS

Maximum Payload:

2,143 LBS

Fuel capacity:

384 GAL

Ownership Costs 2007

Total Cost of Ownership:

$169,656.95

Total Fixed Cost

$108,785.96

Storage:

$840.00

Weather service:

$604.89

Insurance:

$15,139.30

Pilot training

$7,812.00

Miscellaneous expenses:

$1,122.22

Refurbishing and modernization:

$8,776.41

Depreciation:

$74,491.13

Total Variable Cost (58.8 Hrs)
Cost Per Hour = $1,035.22
Cost Per Mile = $3.80

$60,870.99

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

$491.40

Oil cost per hour:

$0.00

Overhaul reserves:

$220.00

Hourly maintenance:

$221.23

Misc: landing, parking, supplies,
catering, etc

$102.59

Engine (x2)

Manufacturer:

Pratt & Whitney

Model:

PT6A-135AÊ

Horsepower:

550 HP

Overhaul (HT):

3,600 Hrs