Beechcraft King Air C90 Gti

The Beechcraft King Air C90 Gti aircraft is build by Beechcraft.

The Beechcraft King Air family is part of a line of twin-turboprop aircraft produced by the Beechcraft Division of Hawker Beechcraft. Model 90 King Air was conceived in 1961. In 1963, Beechcraft began test flights of the proof-of-concept. Beechcraft began accepting orders for the "King Air" in 1963 with deliveries to commence in Autumn 1964.

Beechcraft King Air C90 Gti has a seating capacity of 9, 2 crew and 7 passengers.

Beechcraft King Air C90 Gti has an overall length of 10.82 meters (35.4_ft). Beechcraft King Air C90 Gti has a wing span of 15.32 meters (50.1_ft). The aircraft has an overall height of 4.34 meters (14.2_ft). Beechcraft King Air C90 Gti has a wing area of about 27 sq.meters (290.6_sq.ft.). The overall weight of an empty aircraft is about 3150 kilograms (6,930.0_lbs). And it has a maximum take-off weight of about 4580 kilograms (10,076.0_lbs). Beechcraft King Air C90 Gti can reach a maximum speed of about 500 km/hr (926.0_knots, 804.5_mph). And the Beechcraft King Air C90 Gti has a maximum crusing range of about 2446 kilometers (1,519.9_miles, 1,320.7_nautical miles). Aircraft can reach a service height of about 9144 meters (29,900.9_ft). The aircraft has a stall speed with gears & flaps down: 145 km/hr (268.5_knots, 233.3_mph).

The turboprop engine powered Beechcraft King Air C90 Gti uses 2, Pratt & Whitney Canada PT6A-135APratt & Whitney Canada PT6A-135A. It has a propeller with 2, Hartzell HC-E4N-3N propellers. It can deliver a total power of approximately 820 kilowatts (1,099.6_shaft horsepower).

Updated On: 18.10.15