Beechcraft King Air C90

Overview

The C90 series began in 1971 and incorporated the -20 engine, but in 1976 production switched to the 550shp PT6A-21 and continued with this engine variant through the follow-on C90-1 in 1982.The King Air C90 is found in a variety of configurations, typically six or seven-passenger executive seating with a four-place club, a seat directly across from the airstair door, and a belted lavatory seat. The aft cabin/lavatory area has 26.5 cu. ft. of baggage space. The King Air C90 is powered by a pair of Pratt & Whitney of Canada PT6A-21 turboprop engines flat-rated at 550shp each at ISA +18C. Inspection interval on the engines is 3,600 hours.


Aircraft Specifications


Certified Crew

1

Typical / Maximum Cabin Passenger Capacity

7/9

Balanced Field Length [SL/ISA TMP] (FT)

2275

Length (FT)

35.5

Wingspan (FT)

50.3

Height (FT)

14.3

Cabin Height (FT)

4.8

Cabin Width (FT)

4.5

Cabin Length (FT)

12.7

Baggage Capacity Internal / External (CFT)

48/0

Powerplant

2 P&WC PT6A-21

Years Aircraft Manufactured

1971-1983

Estimated Retail Price Low

290000

Estimated Retail Price High

525,000

Aircraft Category

ME TP < 12,500 LBS



Operating Cost Overview

Aircraft variable and fixed costs are important to determine before making a purchase decisions or planning annual budgets. Our interactive graphs demonstrate the relationships between fuel cost and annual flight hour utilization.



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Range Map

The Beechcraft King Air C90 has a range of 1,151 nautical miles. Type in your city or airport identifier for a visual representation of the NBAA IFR Range (NM) for this aircraft.


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