1965 - 1966 BEECHCRAFT 90 King Air

Twin engine turboprop aircraft with retractable landing gear. The 90 King Air seats up to 9 passengers plus 1 pilot.

Performance specifications

Horsepower:

2 x 500 HP

Best Cruise Speed:

235 KIAS

Best Range (i):

1,270 NM

Fuel Burn:

67.8 GPH

Stall Speed:

75 KIAS

Rate of climb:

2,000 FPM

Rate of climb (1 engine out):

525 FPM

Ceiling:

28,400 FT

Ceiling (1 engine out):

17,700 FT

Takeoff distance:

1,350 FT

Landing distance:

1,250 FT

Takeoff distance over 50ft obstacle:

1,755 FT

Landing distance over 50ft obstacle:

1,870 FT

Weights

Gross Weight:

9,000 LBS

Empty Weight:

5,680 LBS

Maximum Payload:

2,976 LBS

Fuel capacity:

384 GAL

Ownership Costs 1965

Total Cost of Ownership:

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Total Fixed Cost

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Annual inspection cost:

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Storage:

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Weather service:

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Insurance:

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Pilot training

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Miscellaneous expenses:

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Refurbishing and modernization:

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Depreciation:

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Total Variable Cost (100 Hrs)
Cost Per Hour = $749.76
Cost Per Mile = $3.19

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

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Oil cost per hour:

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Overhaul reserves:

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Hourly maintenance:

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Misc: landing, parking, supplies,
catering, etc

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Engine (x2)

Manufacturer:

Pratt & Whitney

Model:

PT6A-6

Horsepower:

500 HP

Overhaul (HT):

3,600 Hrs

Years before overhaul:

None