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Overview

The C90A, introduced in 1984, incorporated an improved cowling design for more efficient air induction and reduced drag, an updated three-bus electrical system, hydraulically actuated landing gear, faired exhaust stacks, and Collins Pro Line avionics installed in a new instrument panel designed to reduce single-pilot workloads. A seven-seat version of the C90A was introduced in 1987, which featured an increase in maximum takeoff weight of 450 lbs., for a total MTOW of 10,100 lbs. In 1992, after a production run of 236 aircraft, the C90A was replaced by the C90B with its four-bladed propellers and significant improvements in cabin noise levels. The King Air C90A is powered by a pair of Pratt & Whitney Canada PT6A-21 turboprop engines flat-rated at 550shp each at ISA +18C. Engine inspection interval is 3,600 hours.


Aircraft Specifications


Certified Crew

1

Typical / Maximum Cabin Passenger Capacity

7/9

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

2577

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)

Powerplant

2 P&WC PT6A-21

Years Aircraft Manufactured

1984-1992

Estimated Retail Price Low

220000

Estimated Retail Price High

230000

Aircraft Category

ME Turboprop



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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If you are further along in the aircraft buying process, our comprehensive aircraft operating cost reports are the perfect companion in your decision making process. View a sample or buy a report and have it available in minutes.




Range Map

The King Air C90A has a range of 1,120 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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