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plus chinook

In this mode it slowly diverged from the direction desired, but was easy to control with the feet where they belong on the pedals. Company testing showed take-off distances of about 300 feet (91 m) on the water and no need for additional vertical surfaces to be added. Packages do not include shipping and handling. Javascript is required to operate this site, Your browser is not compatible with this website. long), Build time: average estimate 180 to 200 hours, Range: 400 statute miles (with two fuel tanks). [15][16], Reviewer Dan Johnson writing in EAA Sport Pilot & Light Sport Aircraft Magazine in January 2008, described the Chinook Plus 2 with the HKS 700E engine:[12], Though the Chinook's wide cockpit gives it a pudgy appearance from some vantage points, the design slips through the air quite well. The yaw axis was interesting – it remained slightly stable with feet on the pedals, but with feet off and the rudder removed from the fin effect as it floated, the aircraft was unstable. In assessing the handling of the 2S one reviewer wrote: Pitch proved to be neutrally stable – it just stayed where it was put. The wing has internal lift and drag bracing wires. These tests resulted in the company billing the aircraft as "Won't Spin". The plane is very responsive to control inputs and exhibits close to neutral static stability in roll. Users may experience limited site functionality. Over 850 in total have been completed and flown and kits remain in production in the 21st century. Website: http://www.capitalairsports.com, Chinook Minnesota Telephone: 320-259-6411 It isn't hard to control, and many aerobatic planes are similarly unstable, but it is an airplane that needs to be flown positively at all times and so would make a less than ideal trainer or plane for a low time pilot. The glide ratio is 10:1 at 35 mph (56 km/h) and minimum sink is 350 fpm (1.78 m/s) at 32 mph (51 km/h). [7], The rights to the Chinook Plus 2 were sold to US company, the Aeroplane Manufactory in 2013, which put the design back into production in 2016. Articles in EAA and related publications: EAA members can digitally view archived editions of Sport Aviation here. The Plus 2 retains the strut-mounted fuel tanks introduced on the 2S. The Chinook Plus 2 typically equipped with a Rotax 582 (65 HP) and is the gold standard in short/soft field capability, useful load, ruggedness, reliability, range and cockpit size with unlimited visibility. Initially ASAP concentrated on supplying parts, but with assistance from the University of Alberta Holomis redesigned the aircraft. They should be easy to build and fix. Chinook Plus 2 airframe body tube, wings, empennage, strut tanks; Complete covering system for wings and empennage; Complete illustrated instructions with help line. The cockpit is of a unique pentagonal cross-section that provides a very wide 38 in (97 cm) cabin at hip level. The pitch and yaw axes both exhibit notable negative static stability and the aircraft likes to diverge from straight and level flight in both pitch and yaw. The WT-11 was the eleventh aircraft designed by Ukrainian-born aeronautical engineer Vladimir Talanczuk, a graduate of the Polish Institute for Aviation Specialists. [2], The remaining flight testing established the service ceiling as 15,000 ft (4,572 m) and the absolute ceiling as 18,400 ft (5,608 m). [2], Test flying the WT-11 was carried out following the first flight on 12 December 1982 at Wizard Lake, Alberta, by company chief test pilot Dennis Maland.

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