Stout Bushmaster 2000

Bushmaster 2000
	Bushmaster 2000 at Oshkosh, Wisconsin, 2005
Role	Airliner
National origin	United States
Manufacturer	Bushmaster Aircraft
First flight	1964
Number built	2
Developed from	Ford Trimotor

The Bushmaster 2000 is a small commuter airliner built in the United States in an attempt to revive the Ford Trimotor design. Work began in 1953 by testing a vintage Trimotor and in 1954 Bill Stout purchased the design rights to the original Trimotor. Due to "Ford Tri-Motor" licensing problems, the Ford 15-AT-D was given the Bushmaster 2000 name.^[1] On 15 January 1955, Stout and partner Robert Hayden from the Hayden Aircraft Corporation announced they were planning to build 1,000 new Bushmasters, but it would be eleven years before the first prototype of the new design flew.

The Bushmaster 2000 featured significant modernization of the original 1920s design, particularly in the choice of materials and construction techniques. It also had more powerful engines, enlarged cockpit windows, a lighter and stronger aluminum-alloy skin, a foot-operated hydraulic replacement of the old Trimotor's hand-operated "Johnny Brake," a larger stabilizer and a dorsal fin to reduce yaw, modern trim tabs and interior rather than exterior control cables.^[2]

However, even with modern engines and propellers, the aircraft's performance did not compare favourably with contemporary designs of similar capacity, and no sales ensued. Combined with financial, management and marketing problems, only two examples were built with a third fuselage never completed.^[1]

The first Bushmaster, N7501V was assembled in 1966, and is owned by Pleasant Aviation LLC At mid America flight Museum and based at Mt Pleasant Regional Airport near Mount Pleasant, Texas. The second aircraft N750RW was completed 18 January 1985 by Ralph Williams, the President of Hydro-Forming in Long Beach, California. This aircraft was written off in an accident at Fullerton Municipal Airport, California on 25 September 2004.^[3]

Specifications

Data from Jane's All the World's Aircraft 1974–75^[4]

General characteristics

Crew: Two
Capacity: 23 passengers
Length: 50 ft 8 in (15.44 m)
Wingspan: 77 ft 11 in (5.0 m)
Height: 13 ft 5 in (4.09 m)
Wing area: 851.7 sq ft (79.13 m²)
Empty weight: 7,500 lb (3,402 kg)
Gross weight: 12,500 lb (5,670 kg)
Powerplant: 3 × Pratt & Whitney R-985-AN-1 Wasp Junior 9-cylinder radial engines , 450 hp (340 kW) each

Performance

Maximum speed: 128 mph (206 km/h, 111 kn) IAS
Stall speed: 55 mph (89 km/h, 48 kn)
Range: 700 mi (1,127 km, 610 nmi)

References

^ ^a ^b O'Callaghan 2002, 124.
^ Time 6 January 1967
^ "National Transportation Safety Board Aviation Accident Final Report Accident Number: LAX04FA330" (PDF). National Transportation Safety Board. July 31, 2006. Retrieved October 31, 2023.
^ Taylor 1974, p. 298

Bibliography

O'Callaghan, Timothy J. (2002). The Aviation Legacy of Henry & Edsel Ford. Ann Arbor, Michigan: Proctor Publications.
O'Leary, Michael (December 2004). "Bushmaster Lost". Air Classics.
"Return of the Tin Goose". Time. 6 January 1967. Archived from the original on 29 May 2011. Retrieved 2008-07-29.
Taylor, John W. R. (ed.). Jane's All the World's Aircraft 1974–75. New York: Franklin Watts, Inc. ISBN 0-531-02747-3.
Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions. p. 225.
World Aircraft Information Files. London: Bright Star Publishing. pp. File 890 Sheet 101.

External links

Media related to Stout Bushmaster 2000 at Wikimedia Commons

[O'Callaghan,_p._124.-1] O'Callaghan 2002, 124.

[Time-2] Time 6 January 1967

[3] "National Transportation Safety Board Aviation Accident Final Report Accident Number: LAX04FA330" (PDF). National Transportation Safety Board. July 31, 2006. Retrieved October 31, 2023.

[jawa74p298-4] Taylor 1974, p. 298

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