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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]
Christen Eagle IIs of the Iron Eagles. Acro Sport I (Homebuilt - 1972) Acro Sport II (Homebuilt) Aircraft Technologies Acro 1 (Homebuilt 1993) Aircraft Technologies Atlantis (Homebuilt - 1996) American Champion Citabria (1964) American Champion Decathlon (1970) American Champion Super Decathlon (1976) Bede BD-8 (Homebuilt - 1980) Beechcraft T ...
(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
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.
Pages in category "Eagle Aircraft" The following 2 pages are in this category, out of 2 total. This list may not reflect recent changes. E. Eagle Aircraft Eagle 150;
The Celair Eagle 300 was a light aircraft with STOL capability [1] developed in South Africa in the late 1980s and early 1990s. [2] Only a single prototype was constructed. Design
Data from Aviat website General characteristics Crew: one Capacity: one passenger Length: 22 ft 7 in (6.88 m) Wingspan: 35 ft 6 in (10.82 m) Wing area: 183 sq ft (17.0 m 2) Empty weight: 1,275 lb (578 kg) on wheels Gross weight: 2,200 lb (998 kg) on wheels and floats Fuel capacity: 50 US gallons (190 litres) Powerplant: 1 × Lycoming O-360-A1P four cylinder, four stroke piston aircraft engine ...
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