Aircraft Description
Background/History
The Beechcraft 65-90 accomplished its first flight in January 1964. Based on the piston-engined Model 65 Queen Air, the -90 featured a pair of the new Pratt & Whitney Canada PT6A turboprop powerplants in place of the earlier Model 65’s Lycoming piston engines. A subsequent pressurized model was developed and designated the King Air 90. Many variants followed including the A90 and B90 powered by the PT6A-20 engine. 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 C90-1 was able to utilize higher ITT limits on the -21 engine due to a strengthened empennage, which resulted in higher cruise airspeeds and improve performance. It also incorporated improved cabin pressurization and a beefed-up airstair door. Before production ceased on the C90 in 1982, 507 aircraft were delivered.
Power
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.
Avionics
The King Air C90 can be found equipped with a variety of avionics including King 900 series dual nav/comm radios, King KDF 800 ADF, and King KXP 755 transponder. More recently, Collins equipment may be installed including dual VHF 20 comms, VIR 30 navs, TDR 90 transponders, ADF 60, DME 40 and Sperry primus 300 color weather radar.
Design Features
The King Air C90 can be found equipped with a variety of avionics including King 900 series dual nav/comm radios, King KDF 800 ADF, and King KXP 755 transponder. More recently, Collins equipment may be installed including dual VHF 20 comms, VIR 30 navs, TDR 90 transponders, ADF 60, DME 40 and Sperry primus 300 color weather radar.
Accomodations
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. Cabin dimensions are 4.8ft. in height, 4.5ft. in width and 12.7ft. in length.
General | King Air C90, BE-C90 | |||
---|---|---|---|---|
Category | Multiengine Turboprop < 12,500 lbs. | |||
Years Aircraft Manufactured | 1971 – 1982 | |||
Serial Number Range | 502 – 1010 | |||
Retail High Price | $1,250,000.00 / 980,875.00€ | |||
Retail Low Price | $300,000.00 / 235,410.00€ | |||
Characteristics | King Air C90, BE-C90 | |||
Seating | 1+7/9 | |||
Wing Loading | 32.8 | |||
Power Loading | 8.8 | |||
Noise(EPNdB): Takeoff/Sideline/Approach | 81.3 | |||
External Dimensions (ft) | King Air C90, BE-C90 | |||
External Length | 35.5 | |||
External Height | 14.3 | |||
External Span | 50.3 | |||
Internal Dimensions (ft) | King Air C90, BE-C90 | |||
Internal Length (Overall/Net Height) | 12.7 | |||
Internal Height | 4.8 | |||
Internal Width (Max/Floor) | 4.5 | |||
Baggage | King Air C90, BE-C90 | |||
External: Cu.Ft./Lb. | N/A | |||
External: Cu.Ft./Lb. | N/A | |||
Power | King Air C90, BE-C90 | |||
Engines | 2 P&WC PT6A-21 | |||
Output (lbs ea.)/Flat Rating | 550shp/ISA+18 | |||
Inspection Interval | 3,600t | |||
Data based on latest manufactured year |