King Air C90

GENERAL CHARACTERISTICS
  • Crew: 2
  • Capacity: 5 Seater
  • Length: 35 ft 6 in (10.82 m)
  • Height: 14 ft 3 in (4.34 m)
  • Maximum Take-off Weight: 10,100 lb (4,580 kg)
  • Powerplant: 2x Pratt & Whitney Canada PT6A-135A turboprops, driving Hartzell HC-E4N-3N propellers, 550 shp (410 kW) each
PERFORMANCE
  • Maximum Speed: 270 kt (500 km/h)
  • Range: 1,321 nm (2,446 km)

The King Air C90 is found in a variety of configurations with typically 5-6 passenger executive seating with a four-place club, a belted lavatory seat and a seat directly across from the air-stair door. The aft cabin/lavatory area has 26.5 cu. ft. of baggage space whereas the cabin dimensions are 4.8ft. in height, 4.5ft. in width and 12.7ft. in length.

This aircraft is a pressurized twin-engine turboprop business aircraft configured as a cantilever low-wing monoplane added with a conventional tail. It utilizes dual bleed air for cabin heat and pressurization. It has hydraulically actuated retractable tricycle landing gear with a single wheel on each unit, and an airstair door on the port side aft of the wing. Leading-edge pneumatic boots provide de-icing of the wing and tail surfaces. The three-bladed propellers are reversible and full-feathering.

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