Rotec Rally Explained
The
Rotec Rally is a family of
American ultralight aircraft that was designed by Bill Adaska in 1977 and produced by
Rotec Engineering of
Duncanville, Texas. Adaska had been an
aeronautical engineer at
Bell Helicopter and the French helicopter manufacturer,
Aerospatiale, prior to starting Rotec. The aircraft was supplied as a kit for
amateur construction.
[1] [2] [3] Design and development
The earliest Rallys were derived from hang gliders and comply with the US FAR 103 Ultralight Vehicles rules, including the category's maximum empty weight of 2540NaN0. The Rally 2, for instance, has a standard empty weight of 1450NaN0. The series all feature a cable-braced high-wing, a single-seat, open cockpit, conventional landing gear and a single engine in pusher configuration. The series was highly successful due to its low price and solid engineering.
The aircraft is made from aluminum tubing, with the flying surfaces covered in Dacron sailcloth. The wing is cable braced from a single kingpost mounted on top of the wing. The tailwheel is sprung.
The first Rallys were simple powered hang gliders and grew in sophistication as the model numbers increased. More than 2000 Rallys were delivered.[3]
Operational history
In reviewing the Rally, All-Aero said:
Variants
- Rally 1
Early powered hang glider model introduced in 1977.[3]
- Rally 2
Improved powered hang glider model with weight shift control for pitch and roll with a seat-cable controlled rudder introduced in 1979. Standard engine is the Solo 210 of 200NaN0. It has a 1450NaN0 empty weight and a cruise speed of 230NaN0.[3]
- Rally 2B
Development of the Rally 2, with a conventional three-axis control system, including wing-mounted ailerons. In production models after 1981 the ailerons were replaced with spoilers for roll control. The control stick on the Rally 2B is hinged from the top, which simplified control runs to the high wing. Standard engine supplied was the Cuyuna 430 two-stroke.
- Rally 3
Two seat version of the Rally 2B, introduced in 1981.[3]
- Rally Sport
Structurally strengthened version of the Rally 2B for aerobatics, with a 2480NaN0 empty weight, 271NaN1 wingspan and glide ratio of 8:1. Introduced in January 1983.[3] Aircraft on display
External links
Notes and References
- Cliche, Andre: Ultralight Aircraft Shopper's Guide 8th Edition, page E-30. Cybair Limited Publishing, 2001.
- Web site: Rally Sport. 8 December 2011. Virtual Ultralight Museum. n.d..
- News: Rotec Engineering. 22 February 2015. 2015. All Aero.
- Web site: Southern Museum of Flight. 8 December 2011. aviationmuseum.eu . n.d..
