Twin engine turboprop aircraft with retractable landing gear. The KING AIR C90B seats up to 11 passengers plus 1 pilot.

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Performance specifications

Horsepower:

2 x 550 HP

Best Cruise Speed:

246 KIAS

Best Range (i):

1,207 NM

Fuel Burn:

88.4 GPH

Stall Speed:

78 KIAS

Rate of climb:

2,010 FPM

Rate of climb (1 engine out):

495 FPM

Ceiling:

30,000 FT

Ceiling (1 engine out):

14,800 FT

Takeoff distance over 50ft obstacle:

2,714 FT

Landing distance over 50ft obstacle:

3,692 FT

Weights

Gross Weight:

10,100 LBS

Empty Weight:

6,950 LBS

Maximum Payload:

2,142 LBS

Fuel capacity:

384 GAL

Ownership Costs 1992

Total Cost of Ownership:

$150,776.61

Total Fixed Cost

$57,035.51

Storage:

$840.00

Weather service:

$604.89

Insurance:

$8,624.59

Pilot training

$7,812.00

Miscellaneous expenses:

$822.55

Refurbishing and modernization:

$4,999.76

Depreciation:

$33,331.73

Total Variable Cost (100 Hrs)
Cost Per Hour = $937.41
Cost Per Mile = $3.81

$93,741.10

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

$477.09

Oil cost per hour:

$0.00

Overhaul reserves:

$234.00

Hourly maintenance:

$133.42

Misc: landing, parking, supplies,
catering, etc

$92.90

Engine (x2)

Manufacturer:

Pratt & WhitneyÊ

Model:

PT6A-21

Horsepower:

550 HP

Overhaul (HT):

3,600 Hrs