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 Characteristics


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

General Information


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

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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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