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Beech B90 King Air


The Model B90 King Air superseded the Model A90 in 1968 and differed from its predecessor in a number of ways. It had an increased wingspan, the same as the Queen Air A80, and a remodeled rear fuselage. It also featured improvements to the pressurization system, flight instruments and the aileron system.

 OY-JRO                    c/n LJ-327                    USA  
10 seat business aircraft first flown in 1967

Engines: 2x 550shp(410kW) Pratt & Whitney PT6A-2
Length: 35’6”(10.82m)                                                                                         Height: 14’3”(4.34m)
Wingspan: 50’3”(15.31m)                                                                                               No.built: 181
Range: 1480miles(2381km)                                                              Cruising speed: 260mph(418kmh) Empty weight: 5685lb(2580kg)                                              Maximum take-off weight: 9650lb(4381kg)

The aircraft shown above is a cargo conversion of the B90. The aircraft illustrated next is a standard version.

                                      N984AA                       c/n LJ-429

The Model C90 King Air (496 built) was introduced in 1971 and was powered by 2X 550shp(410kW) P&W PT-6A-21 engines. The C90’s cabin pressurization was changed from supercharger to an engine bleed system. Apart from these changes it was similar to the Model B90. Two examples of the Beech C90 are illustrated below.

                                      F-GCLD                      c/n LJ-637

                                      LN-KCG                   c/n LJ-768     

An improved version of the Model C90 was the Model C90-1 (47 built) which was introduced in 1982. It featured the strengthened tailplane of the Model E90 and improved cabin pressurization. An example of the Beech C90-1 King Air is illustrated below.

Beech C90-1 King Air

                                      N6723Y                  c/n LJ-1013

The Model C90-1 was quickly superseded by the Model C90A (228 built) which was first flown in 1983. It featured high-efficiency ‘pitot cowl’ engine nacelles where the air inlet area is reduced to about half that on preceding models. An example of the C90A is shown below.

                                      N724KH                  c/n LJ-1426

The Model C90A began with c/n LJ-1063 onward. Other improvements to the C90A included faired exhaust stacks and an hydraulically actuated undercarriage retraction system, rather than the previous electrically operated system. In 1991 Beech introduced the Model C90B (93 built) which featured a number of improvements over the Model C90A including four-bladed propellers. The Model C90B remains in production. An example of the Beech C90B King Air is illustrated below.

Beech C90B King Air

                                        N5154E               c/n LJ-1655

Two other variants of the Model C90B also remain in production. The Model C90B Special Edition which was introduced in 1994 and is a less expensive version, and the Model C90B Jaguar Special Edition introduced in 1998. The Jaguar Special Edition involves an aesthetic make-over for the aircraft at a cost of around $70,000 US. This involves a new Jaguar green and gold colour scheme with the Jaguar motif, burl walnut trim and Connoly leather upholstery. Production of the Model C90 continues with the C90GT (66+ built) which has a maximum take-off weight of 10,100lb(4581kg). More than 1830 Model B/C series aircraft had been built by early 2007. An example of the Jaguar Special Edition is illustrated below.

                                      N38XJ                    c/n LJ-1512

 

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