rutan quickie aircraft for sale

Rutan Quickie Aircraft For Sale - As a low-power, high-performance gear plane. Its tandem wing design has a single anhedral front wing and a slightly larger dihedral rear wing. The front wing has full control surfaces and is thus similar to a canard wing, but considerably larger. The aircraft has an unusual undercarriage, with the main wheels located on the front wingtips.

Quickie Aircraft Corporation was formed after 1978 to produce and sell the Quickie in kit form. A two-seater variant of the same layout as the Q2 two years later. The original Quickie (model 54 in the Rutan design series) is one of several unusual aircraft that Rutan produced for the general aviation market.

Rutan Quickie Aircraft For Sale

The Quickie followed Jewett and Sheehan's 1975 vision for a low-cost, low-engine, single-seat home-built aircraft. The first element that Jewett and Sheehan found was the engine, which - although insufficiently powerful (they expected 12 horsepower) - had to be reliable for aviation work. Thanks to the industrial four-stroke engine manufacturer Onan, they buy 70 hp. (32 kg), which can deliver 18 hp. (14 kW) at 3,600 rpm.

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Rutan participated in the design; Sheehan and Jewett present an expanded Vari-Ez. After the initial thrust-canard configuration design (Rutan Model 49) was abandoned,

The solution to its towing problems was a tractor genie/tandem wing arrangement, with no tow truck and a viable towing travel ratio.

In contrast to the canard layout, the convention-facing layout brings the pilot closer to the center of gravity for a light aircraft. Many wheels were fitted with wing casings and the tandem layout provided safe stopping features.

Rutan drew the first drawings in May 1977, then the three worked on design drawings for the next two months, with construction starting in August.

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After the first flights, Rutan spent more time on his Defiant design and other projects, and Jewett and Sheehan continued to develop the design and marketed it for domestic use.

An agreement was reached that Rutan would finance the development and testing, and once the design was complete, they would pay Rutan from the sale of designs and tools.

The Quickie is a tandem-wing tail glider with one front wing and one rear wing (instead of the usual main wing and tail). According to Rutan, this arrangement is not new, it was previously used on aircraft such as the Flying Spur Migneto.

As with other Rutan designs, the Quickie is constructed of fiberglass and resin with a foam core. The wings are foam blocks cut to shape with hot wire before being sheathed, and the fuselage is made from 1-inch-thick (25.4 mm) foam slabs.

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Full-length control surfaces on the front wing act as combined elevators and flaps. The ailerons are located on the rear wing, facing away from the pilot. Tandem arrangement

Provides positive lift of both pairs of wings; while in an airplane, the propeller provides mostly negative lift.

Cookie installed the main (non-retractable) main wheels in holes located at the front wing tips. The lack of a separate landing gear helps reduce weight and drag,

Such savings that allow a smaller engine and smaller fuel consumption. Although the propeller has a small diameter, propeller clearance remains limited and the Quickie is prone to ground strikes.

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The pilot controller has a stick on the right and a throttle on the left. The rudder pedals are connected to the steerable tail. Cable-operated brakes consist of a cockpit lever operating steel tire cleaners on each main wheel.

The Quickie prototype, registered "N77Q" (77 for 1977, Q for Quickie.) began the flight test program in November 1977. All three designers flew it on the first day. The prototype was modified during the test program. Both the canard and main wing were increased in length to improve maneuverability. This reduced stall speed and shortened takeoff and landing distances.

At first only a beautiful tail was designed with a fixed fin and worked as a rudder, replacing the rudder. A rudder-controlled tail allows directional control at the point of take-off, as the Quickie does not raise its tail in flight. Although it takes off at 55 mph and has a top speed of 126 mph, its rate of climb is "modest."

In June 1978, the Quickie prototype was flown to the Experimental Aircraft Association's annual meeting at the EAA AirVture Oshkosh in Oshkosh, Wisconsin, where the aircraft attracted public interest and won the Outstanding New Design Award.

Airplane Design (green/orange)

In June 1978, two months after the first flight of the prototype, Jewett and Sheehan formed Quickie Aircraft Corporation to produce and sell complete aircraft kits. Production began in June 1978, and by 1980 the company had sold 350 sets. Other companies were given marketing rights, and eventually about 1,000 Quickie kits were sold. In 1975, Gene Sheehan and Tom Jewett began searching for a small, reliable engine to power small, efficient, sport utility aircraft. After many tests, they decided that the 13.4 kW (18 hp) Onan industrial engine of aluminum construction was ideal for this purpose. In 1977, men introduced the revolutionary Vari-Wigen, VariEze, etc. It would be easy enough to approach designer Bert Rutan to design an airplane that would produce the desired performance with fuel economy.

The design challenges are mainly due to low strength and the need to keep overall weight to a minimum. Later a tractor canard/tail less biplane configuration was used, where the pilot sits near the center of gravity, and the main fuselage covers the canard surface. A full-length elevator/flap was mounted on the canard inboard of the ailerons on the rear wing, and the tail chain acted as a rudder. Construction of the prototype began in August 1977 and after 400 hours it first flew on 15 November. A short test flight revealed that the tail meat was inadequate and a conventional fin and rudder were added.

The aircraft was soon named "Cookie" for its cruising speed and speed of construction. The machine is constructed from a low density rigid foam fiber sandwich which forms the core material. The structure is built directly based on the shape, thus reducing the construction time and providing many other important features.

With a 91 kg (200 lb) pilot, the Quickie Q-1 can travel 804 km (500 mph) with a top speed of 185 km (115 mph). 145 km/h cruise (90 mph) fuel consumption 35.75 km per liter (100 mpg).

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The Quickie Q-1 was developed as the QQ-100, later the Q-2 and the Q-200 two-seater variant (developed separately). Q-2 The Q-1 was originally designed by Canadian Harry Le Gare in 1980 and first flew on July 1, 1980. Typically powered by a 56 kW (75 hp) Revmaster 2100 DQ engine. . The wingspan remained the same as the Q-1, but the wing area was increased to 6,224 m² (66.99 sq mi) and the cruise speed was 252 km/h (156 mph), with 75% power at 1,092 rpm. km (679 mi), and weighs 499 kg (1,100 lb). Payload was 227 kg (500 lb).

A variant of the Q-2 was the Q-200, introduced in 1982, powered by a 75 kW (100 hp) Continental O-200 engine and cruising at 306 km/h (75 mph) at 75% power. There is also the option of cycling. More than 500 Q-1s and more than 1,000 Q-2s and Q-200s were sold in kit form. Eight examples of the series were registered in Australia and four in New Zealand.

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