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Beech Kingair C90A (VT-RSL)
RSL
Flaps Aviation Private Limited
Class: Turboprop Aircraft
Max. Passemgers: 6
Facilities : Entertainment system
Aircraft Specification
No of Engines : 2
Engine Mfg: Pratt & Whitney Canada
Max Speed: 250 Kts
Max Range: 1125 NM
Cabin Height: 4 ft 10 In
Cabin Length: 12 ft 5 In
Cabin Width: 4 ft 6 In
Cabin Volume: 227 cu ft
Door Height: 4 ft 3 In
Max T/O Weight: 10100 LB
Max Payload: 3100 LB
About Aircraft
Beech Kingair C90A (VT-RSL) The Beechcraft King Air family is part of a line of twin-turboprop aircraft produced by Beechcraft. The King Air line of aircraft is comprised of a number of models that have been divided into two families; the Model 90 and 100 series are known as King Airs, while the Model 200 and 300 series were originally marketed as Super King Airs. Since production began in 1964, over 3,100 aircraft have been built. Production is currently still active, giving the Beechcraft King Air the longest continual production run of any civilian aircraft of its class. Several variants of the original design were created, including the Model A90, B90, and C90. The Model C90A, a variant of the C90, was introduced in 1984.
The Model C90A featured the redesigned engine cowlings of the F90-1 and received an increase in takeoff weight in 1987, being certified to 10,100 lb. The aircraft was equipped with improved C90-1 landing gear retraction and electrical systems. It is powered by two Pratt & Whitney PT6A-21 turboprop engines with 550 shp each.
Production of the King Air C90A ended in 1992, with a total of 235 being built.
Disclaimer: Information on this site may not be accurate or current and is not valid for flight planning or any other aircraft operations. No warranty of fitness for any purpose is made or implied. Flight planning or any other aircraft operations should only be done using official technical information provided by the manufacturer or FAA.
Disclaimer
Information on this site may not be accurate or current and is not valid for flight planning or any other aircraft operations. No warranty of fitness for any purpose is made or implied. Flight planning or any other aircraft operations should only be done using official technical information provided by the manufacturer or FAA.