The aircraft in the series all feature one or two seats, fixed conventional landing gear and a single engine in tractor configuration. The Acrolite fuselages are all made from welded 4130 steel tubing, with wooden structure wings covered in hot laminated plywood and control surfaces made from aluminum sheet. All other surfaces are covered in dopedaircraft fabric. Wing arrangements, cockpit and engines vary by model.[1][2]
The Acrolite 1A won a Canadian Owners and Pilots Association "Good Show" award in 1998 and the Acrolite 1B was chosen as one of two finalists in the 1995 Aircraft Spruce & Speciality Scratchbuild Design Contest.[3][4][5]
Single-seat biplane for the Canadian basic ultralight category, first flown in October 1986. Plans no longer available. The prototype was originally powered by a 38hp (28kW)Kawasaki 440 and later by a 40hp (30kW)Rotax 447two-strokes powerplant.[4][8]
Acrolite 1B
Single-seat biplane for sportsman aerobatics. In addition to the standard wooden wing, optional 2024-T3 aluminum sheet wings can be built. The recommended engine is the 80hp (60kW)Rotax 912UL, although the 64hp (48kW)Rotax 582or the 120hp (89kW)Rotax 618 two-strokes can be used as well.[1][5][8]
Single-seat high-wing, strut-bracedmonoplane. Engines include 40hp (30kW)Rotax 447, 50hp (37kW)Rotax 503 and the 64hp (48kW)Rotax 582 two-strokes or other similar powerplants. Acrolight Aircraft reports that no prototype has been completed or flown by September 2012.[8][10]
Acrolite 1T
Single-seat triplane for sportsman aerobatics, with wings covered with epoxyfiberglass sheet or optionally plywood. Ailerons are only fitted to the middle wing. Engines include 40hp (30kW)Rotax 447, 50hp (37kW)Rotax 503 and the 64hp (48kW)Rotax 582 two-stroke powerplants.[1][2][8][11]
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