;Acrolite 1A :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
Kawasaki 440 and later by a
Rotax 447 two-strokes powerplant. ;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
Rotax 912UL, although the
Rotax 582or the
Rotax 618 two-strokes can be used as well. ;Acrolite 1M :Single-seat high-wing,
strut-braced monoplane. Engines include
Rotax 447,
Rotax 503 and the
Rotax 582 two-strokes or other similar powerplants. Acrolight Aircraft reports that no prototype has been completed or flown by September 2012. ;Acrolite 1T :Single-seat
triplane for sportsman aerobatics, with wings covered with
epoxy fiberglass sheet or optionally plywood.
Ailerons are only fitted to the middle wing. Engines include
Rotax 447,
Rotax 503 and the
Rotax 582 two-stroke powerplants. ;Acrolite 2M :Two seats in
tandem, high-wing strut-braced
monoplane intended for the Canadian
advanced ultralight category and American
light-sport aircraft category, first flown in June 1994. Engines include
Rotax 582,
Rotax 618 two-strokes and the
Rotax 912UL and
Jabiru 2200 four-stroke powerplants. As of August 2012, the design does not appear on the
Federal Aviation Administration's list of approved special light-sport aircraft or on Transport Canada's list of advanced ultralights. ==Specifications (Acrolite 1C) ==