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Christen/Aviat Eagle II Most common variant, two seat dual controls. Lycoming AEIO-360.200 hp (150 kW) The first Eagle II produced (Serial #001) is on display at the Connecticut Air & Space Center in Stratford, CT. [5] Christen Super Eagle I 540 Two built. Lycoming AEIO-540 300 hp (220 kW).
[4] [5] The company then designed and manufactured the Christen Husky A-1 utility aircraft. In 1990, the company was the subject of a lawsuit claiming that the design of their aircraft was responsible for the death of a pilot. [6] Christen Industries was, in turn, bought by Aviat Aircraft, Inc. in 1991, who continued both product lines. [7] [8]
(1926:Central States Aero Co Inc, Wallace Field, Bettendorf, IA, 1927:Renamed Central States Aircraft Co. 1928:Reorganized as Mono Aircraft Co, Moline, IL) Central States Monocoupe 22 [ 1 ] Central Washington
Three Canadair CL-215 amphibious flying boats. The following is a list of seaplanes, which includes floatplanes and flying boats.A seaplane is any airplane that has the capability of landing and taking off from water, while an amphibian is a seaplane which can also operate from land.
Data from Cliche. General characteristics Crew: one Wingspan: 35 ft (11 m) Wing area: 177 sq ft (16.4 m 2) Empty weight: 225 lb (102 kg) Gross weight: 1,023 lb (464 kg) Fuel capacity: 4 U.S. gallons (15 L; 3.3 imp gal) Powerplant: 1 × Cuyuna 430R twin cylinder, two-stroke aircraft engine with 2.2:1 cog-belt reduction drive, 35 hp (26 kW) Propellers: 2-bladed wooden, 5 ft 6 in (1.68 m ...
Certified versions of the Pitts are now produced by Aviat Aircraft in Afton, Wyoming.It is available as the S-1 single-seater with an up to 200 hp (150 kW) flat-4 Lycoming engine and a 17 ft 4 in (5.28 m) wingspan, or as the S-2 two-seater variant featuring a 260 hp (194 kW) flat-6 Lycoming and a 20 ft (6.1 m) wingspan.
The DW.1 was designed by Dean Wilson of the Eagle Aircraft Company of Boise, Idaho and the first example first flew in 1977. The Eagle is a single-seat agricultural biplane with tapered long-span wings, an enclosed single-seat cockpit and fixed tailwheel undercarriage.
The aircraft is made from aluminum sheet. Its 28.5 ft (8.7 m) span wing has an area of 135 sq ft (12.5 m 2) and features electrically operated flaps. The standard engine is the 100 hp (75 kW) Rotax 912ULS four-stroke powerplant [1] while the standard propeller is a Sensenich composite ground adjustable type. [4]