Twin engine turboprop aircraft with retractable landing gear. The KING AIR C90GT seats up to 9 passengers plus 1 pilot.

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Performance specifications

Horsepower:

2 x 550 HP

Best Cruise Speed:

270 KIAS

Best Range (i):

1,026 NM

Fuel Burn:

65.7 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:

3,372 FT

Landing distance over 50ft obstacle:

3,060 FT

Weights

Gross Weight:

10,100 LBS

Empty Weight:

7,150 LBS

Maximum Payload:

1,934 LBS

Fuel capacity:

384 GAL

Ownership Costs 2005

Total Cost of Ownership:

$187,719.41

Total Fixed Cost

$95,370.39

Storage:

$840.00

Weather service:

$604.89

Insurance:

$13,516.22

Pilot training

$7,812.00

Miscellaneous expenses:

$1,047.56

Refurbishing and modernization:

$7,835.49

Depreciation:

$63,714.22

Total Variable Cost (100 Hrs)
Cost Per Hour = $923.49
Cost Per Mile = $3.42

$92,349.02

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

$354.62

Oil cost per hour:

$0.00

Overhaul reserves:

$278.00

Hourly maintenance:

$199.36

Misc: landing, parking, supplies,
catering, etc

$91.52

Engine (x2)

Manufacturer:

Pratt & Whitney

Model:

PT6A-135A

Horsepower:

550 HP

Overhaul (HT):

3,600 Hrs