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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). Formerly flown by the Iron Eagles aerobatic team, now owned by Professional Pilots based in Texas and Alaska. Christen Super Eagle II
[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 Industries Inc (Fdr: Frank L Christensen), Hollister, CA, 1991: Acquired by Aviat Aircraft Inc, Afton, WY) Christen Eagle I; Christen Eagle II; Christen Husky;
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 ...
In 1979, aircraft designer Frank Christensen invited the team to test fly a new aerobatic aircraft he had designed: the Christen Eagle. The Devils were so impressed that they switched their team aircraft to the Eagle, and renamed the Red Devils to the Eagles Aerobatic Team, [5] with Charlie Hillard as the lead pilot. The Eagles Aerobatic Team ...
Aviat Aircraft Cessna 152. The company was founded in 1991 based on the history of the Call Aircraft Company and the product lines of the Pitts and Christen companies. [2] [3] In 1995, the company was purchased by Stuart Horn and renamed Aviat Aircraft Incorporated.
Celliers' plans for the Eagle were to obtain American FAR 23 and South African DCA certification [2] and to put it into production by 1992. [2] [4] [5] By 1993, development had ceased and Celair was out of business. [7] In February 1993, the rights to the Eagle design were put up for sale. [3]
Data from Lambert & Munson 1994, p.6 General characteristics Crew: One pilot Capacity: 1 passenger Length: 6.53 m (21 ft 5 in) Wingspan: 7.15 m (23 ft 5 in) Height: 2.26 m (7 ft 5 in) Wing area: 5.02 m 2 (54.0 sq ft) Empty weight: 327 kg (721 lb) Max takeoff weight: 567 kg (1,250 lb) Powerplant: 1 × Teledyne Continental IO-240 -A four-cylinder, horizontally-opposed, air-cooled piston engine ...
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