In Australia the A-32 is referred to as the Vixxen.

The A-32 is a development of the A-22 Foxbat; however unlike the earlier aircraft, which can be purchased in kit form or fully assembled, the A-32 Vixxen is supplied only as a kit in the UK, or ready-to-fly factory-built aircraft in 31 other countries.

To increase cruise speed while employing the same 100 hp (75 kW) Rotax 912ULS engine as the A-22, the A-32 has a new flush wing-to-body fairing design and all flying horizontal stabilizer, as well as moulded baffling for improved engine airflow and cooling. Other changes include a wing that is 10 cm (3.9 in) shorter, shorter lift struts and better wing tank fairing. This results in a cruise speed that is 20 kn (37 km/h) faster than the A-22.

The prototype A-32 was completed in January 2014 and the first production aircraft was shown in April 2015. It was then transported to Australia, first flying at Moorabbin on 20 July 2015.

Variant.

Aeroprakt A-32L

An ultralight variant of the A-32 with a MTOW of 450 kg (or 472.5 kg with recovery parachute system) to comply with European regulations, although not UK legal. Central control Y-stick installed as default, twin control yokes offered as an option.

For manufacturers website, click here.

The aircraft was designed to comply with the Fédération Aéronautique Internationale microlight rules, US light-sport aircraft rules and UK BCAR Section "S". It features a cantilever low-wing, a two-seats-in-side-by-side configuration enclosed cockpit, fixed or retractable tricycle landing gear and a single engine in tractor configuration.

The aircraft is made with carbon fibre sandwich construction. The cockpit width is 1.15 m (45 in). Standard engines available are the 100 hp (75 kW) Rotax 912ULS, the Rotax 912iS[4] and the 115 hp (86 kW) Rotax 914 four-stroke powerplants. A glider towhook is optional equipment.

The aircraft is supplied as a complete ready-to-fly-aircraft.

The design has been developed into a three to four seat aircraft, the Aerospool WT10 Advantic.

Variants

Microlight version

Base model with gross weight of 450 kg (992 lb) and 75 litres (16 imp gal; 20 US gal) fuel capacity for the European microlight category.

LSA version

Model with gross weight of 549.7 kg (1,212 lb) and 98 litres (22 imp gal; 26 US gal) fuel capacity for the US light-sport aircraft category. Standard empty weight is 299.5 kg (660 lb), useful load 250.5 kg (552 lb), range 1,397 km (868 mi).

Dynamic Club

EASA Type Certified Model in Restricted airworthiness category to meet Certification Specification CS-LSA, two-seats with fixed landing gear and powered by a Rotax 912 ULS2.

Specificatons below are for the WT9 Dynamic European microlight version.

For more extensive performance data,, click here.

The Aerosport Quail is an ultralight aircraft that was designed for home building by Harris Woods. First offered for sale in 1971, by the end of the decade, 375 sets of plans had been sold, with around 26 aircraft under construction and 10 flying.

The Quail is an all-metal cantilever high-wing monoplane with an enclosed cabin and tricycle undercarriage. The aircraft uses simple flat-sided construction with pop-rivet assembly. The wing design is unmodified from the Aerosport Rail homebuilt. The prototype was powered with a Rockwell L680R engine.

The Aerosport Scamp A is a small biplane designed for home building by Harris Woods. It featured an open cabin, tricycle undercarriage, and a T-tail.

The Scamp A first flew on August 21 1973, powered by an 1853 cc Volkswagen car engine. 1,050 sets of plans had sold by 1993. In addition to the many examples which have been completed in the United States, several examples of the type are active in the United Kingdom.

The Agrocopteros Scamp B is an agricultural crop spraying version of the Scamp, modified from kits assembled in Columbia.

Seating two persons in tandem in open cockpits, the Woody Pusher had a parasol wing and was a light aircraft aimed at the homebuilt market for sport use. Construction was of braced wooden wings with a metal leading-edge and fabric covering overall. The fuselage was a welded steel-tube structure with fabric covering. The tail unit was braced and the undercarriage was non-retractable. The engine was installed in the pusher configuration.

Designed with the amateur builder in mind, the prototype Woody Pusher’s fuselage was wood with plywood covering, and then with fabric covering overall. Subsequently the designer, Mr Harris L Woods, decided to re-design the fuselage and undercarriage. The type was marketed by Aerosport Inc of Holly Springs, North Carolina, USA. The prototype first flew with a 48 kw (65 hp) Lycoming engine but was later re-engined. Provision was made for engines in the 48 kw (65 hp) to 63 kw (85 hp) range to be installed.

At least one Woody Pusher has been built in New Zealand, being built by Alan Belworthy and completed as ZK-DUA (c/n AACA/172) in November 1974. It was involved in an accident on 27 January 1980. It was restored, was powered by a Continental A-75 four-cylinder engine, and in later years has been operated from an airstrip at Cust.

One on display at the Wings Over the Rockies Air and Space Museum, Denver, Colorado, with a 75-hp Continental engine (No. N393EA). Another, N100FQ, is displayed at the Florida Air Museum, Lakeland, Florida.

Archon SF-1 is an evolutionary unique aircraft, that utilizes the look of a modern fighter aircraft but lies into the Ultalight(EU)/LSA(USA) category. The idea behind the design is an affordable recreational aircraft that offers the impression and the feeling of a fighter aircraft.

It was designed and built in Greece, by George Iliopoulos. The maiden flight was made in July, 2009. Since then, it’s been being test flown in regular basis and have received minor changes to improve the overall flight qualities. 

The standard engine mount is for the Rotax 503, 532, 582 engines.Alluminum alloy construction, light-weight and durable material, corrosion resistant, UV protected. Easy to work with.Basic skills and tools required to assemble in a small workshop.

The aircraft is supplied as a complete ready-to-fly-aircraft.

The aircraft was designed to comply with the Fédération Aéronautique Internationale microlight, and US light-sport aircraft rules. It features a cantilever low-wing, a two-seats-in-side-by-side configuration enclosed cockpit, fixed tricycle landing gear and a single engine in tractor configuration.

The aircraft is made from aluminum sheet. Its 9.17 m (30.1 ft) span wing employs manually operated flaps. The standard engine is the 100 hp (75 kW) Rotax 912ULS four-stroke powerplant, driving a three-bladed Woodcomp propeller.

Variants
R40F
     Initial ultralight model
R40FS
     Improved model
R40S
     Base model with dial instruments[4]
R40S-GC
     Version for IFR flight, with a Dynon Skyview glass cockpit

Specifications below are for the R40F/FS Festival.

Designed and built in Germany, it meets both European and US light light-sport aircraft requirements and has been in production since 2001.

It is a conventionally laid out low wing ultralight, seating two side by side. It is largely constructed of riveted aluminium, with composites only used for non-structural fairings and the undercarriage.

The wings have constant chord and slightly upturned trailing edge tips. Mass balanced, half span Fowler flaps immediately inboard of the ailerons may, as an option, be electrically driven. The fin and rudder are swept and straight edged apart from an initially curved leading edge fillet. The rudder is deep and moves in a cut-out in the separate elevators. The tailplane has constant chord. Both elevators and rudder are horn balanced; there is a trim tab on the port elevator.

Breezer Light Sport aircraft exhibited at the Sun 'n Fun show at Lakeland Linder International Airport, Florida, in 2011

The cockpit, located over the wings, has a large hinged canopy and fixed separate windscreen. The Breezer has a tricycle undercarriage with spatted wheels mounted on composite sprung cantilever legs fixed to the lower fuselage. The nosewheel is steerable. A ballistic parachute is an option: either a Junkers or a BRS 5UL type may be fitted.

For more informaton including the seven variants, click here.

Specifications below are for the Rotax 912 ULS version.

Designed by Dave Edwards, it is intended for amateur construction. The aircraft plans claim it can be built out of readily sourced and inexpensive materials using common tools in 150 to 250 hours construction time.

The Affordaplane is constructed of an 6061 T-6 aluminum tube fuselage and other structural components, using both square and round aluminum tube. Wings are a "ladder-type" cross-brace structure supported by struts and covered in doped fabric. Builders have the option of constructing the ribs out of aluminum tube or rigid foam. Instead of welding, structural components are attached with riveted or bolted aluminum gussets. The cockpit is exposed with a plexiglass or Lexan windshield. The controls are conventional 3-axis.[citation needed]

When built as a Part 103 ultralight, the aircraft is intended to be powered by a 26 hp (19 kW) Rotax 277, 35 hp (26 kW) Rotax 377, or similar engine. Heavier and more powerful engines including the Rotax 503 may also be used, but will result in exceeding the FAR Part 103 254 pound (115 kg) empty weight limit, if the aircraft is otherwise built as designed. The plans recommend Rotax engines, but the Half VW, Kawasaki 340 and Kawasaki 440 have also been used.

The Affordaplane has a unique single acting aileron control surface approximately the entire length of the wing. Some builders have configured these as flaperons but the plans do not include details for this modification.

The Airkraft Sunny is an ultralight aircraft that was designed by Dieter Schulz. The aircraft was initially produced by his company, Tandem Aircraft KG of Saulgau, Germany, which built about 150 examples between 1989 and 1999. After he sold the rights in 1999, it was then produced by Dewald Leichtflugzeugbau Gmbh of Bad Schönborn, Germany and more recently by Airkraft Gmbh Leichtflugzeugbau of Beringen, Switzerland, who seem to have gone out of business in about 2010 and production ended. Originally supplied ready-to-fly, later the aircraft was supplied as a kit for amateur construction or as a complete ready-to-fly-aircraft.

The aircraft complies with the Fédération Aéronautique Internationale microlight category rules. It features an unusual diamond-shaped biplane, strut-braced closed wing layout, a two-seats-in-tandem enclosed or open cockpit, fixed tricycle landing gear and a single engine in pusher configuration. The upper wing is swept back, while the lower wing is straight, but mounted further aft. The two wings are joined by swept tip rudders. The elevons are mounted to the lower wing only.

The aircraft is made from bolted-together aluminium tubing, with its flying surfaces covered in Dacron sailcloth. Standard engines available include many models of Hirth, Rotax, BMW and Verner 133M powerplants, ranging from 65 to 80 hp (48 to 60 kW).

Variants

Sunny Light   (Specifications below)
Version with open cockpit
Sunny Sport
Two seat tandem version with enclosed or semi-enclosed cockpit
Sunny Side-By-Side
Version with side-by-side configuration seats
Sunny Targa
Fully enclosed version.
Sunny Amphibian
Version with amphibious floats

The AirLony Skylane UL is a Czech two-seat, microlight, cabin monoplane manufactured by AirLony of Štětí.

The AirLony Skylane design was inspired by the much larger four-seat Cessna 182 Skylane, which it greatly resembles. The manufacturer calls it a "small Cessna".

The Skylane is a high-wing monoplane with a fixed nose-wheel landing gear and powered by a Rotax 912 piston engine. The enclosed cabin has side-by-side seating for two and dual yoke-style controls.

The aircraft is built from a combination of wood and composites. The fuselage is of composite construction, while the strut-braced wing is of wooden structure with a semi-laminar MS (1)-313 airfoil and features a D-cell. The wing is fabric-covered and has two integral 42 l (11 US gal) fuel tanks. The wooden structure, fabric-covered and electrically operated flaps cover 39% of the wing chord and can be lowered to fixed positions of 13°, 29° and 37°.

The tail fin is of wood construction and features a NACA 0012 symmetrical airfoil. The main landing gear legs are made from fibreglass laminates and mount wheels with hydraulically operated toe-brakes. The nose wheel is of a fully castering design and can rotate 360°, allowing the aircraft to be pushed backwards while ground handling.

The Skylane can use engines from 50 to 100 hp (37 to 75 kW) with engine weights of 50 to 100 kg (110 to 220 lb), including the Rotax 912ULS, Jabiru 2200 and Volkswagen air-cooled engines.

Extracts from flight review on bydanjohnson.com. Click link for full review.

Created by Brazil’s AirMax Construcoes Aeronaticas, the SeaMax is designer Miguel Rosario’s 22nd design and his experience shows. The M-22 is very well thought out with many details not present in other LSA.

The SeaMax M-22 appears physically small from the outside.With the wing chesthigh for most people, the SeaMax looks tinier than it is and the light weight surely contributes much to the relative high performance of this flying boat. Light and small it may seem, but when you step inside, you’ll find the interior to be surprisingly
roomy.

Entire airframe made of composite materials including fiberglass, carbon fiber, and Kevlar; steel or stainless
steel landing gear and other components; made in Brazil with numerous parts American sourced; distributed in American by Florida-based company.

The I-11 was a two-seat civil utility aircraft manufactured in Spain in the 1950s. Originally designed by the Spanish aircraft company Iberavia, its first (of two) prototype flew on 16 July 1951. It was a low-wing monoplane of conventional configuration with fixed, tricycle undercarriage and a large, bubble canopy over the two side-by-side seats. Flight characteristics were found to be pleasing, but before plans could be made for mass production, Iberavia was acquired by AISA.

The new management decided to continue with development, but made a few changes to the design, reducing the size of the canopy, and replacing the undercarriage with a taildragger arrangement. This configuration entered production in 1952 with an order from the Director General for Civil Aviation for 70 aircraft for use in Spain's aeroclubs. The Spanish Air Force then ordered 125 for use in training and liaison roles.

The Air Force then requested 200 aircraft built with the seats in tandem, which were designated I-115 by the manufacturers powered by a 112 kW (150 hp) ENMA Tigre inverted air-cooled engine.Number built    208

Variant

I-11
2 prototypes by Iberavia, tricycle undercarriage
I-11B
Production examples by AISA
AISA I-115
Tandem-seat version.

The Alisport Yuma is an Italian ultralight aircraft, produced by Alisport of Cremella. The aircraft is supplied as a kit for amateur construction or as a complete ready-to-fly-aircraft.

Zenith Aircraft considers the Yuma an unauthorized copy of the Zenith STOL CH 701. The World Directory of Light Aviation describes it as being inspired by the CH 701.

The aircraft was designed to comply with the Fédération Aéronautique Internationale microlight rules. It features STOL performance, a strut-braced high-wing, a two-seats-in-side-by-side configuration enclosed cockpit, fixed tricycle landing gear and a single engine in tractor configuration.

The Yuma's fuselage is made from welded steel tubing, covered in aluminium sheet and the tail surfaces covered in doped aircraft fabric. The wing is all-aluminium, with its leading edge slats made from carbon fibre. Its 9.75 m (32.0 ft) span wing employs V-struts, jury struts and flaps. Standard engines available are the 80 hp (60 kW) Rotax 912UL, the 100 hp (75 kW) Rotax 912ULS and the 115 hp (86 kW) Rotax 914 turbo-charged four-stroke powerplant.

The Pioneer 200 was designed to comply with the Fédération Aéronautique Internationale microlight rules and US light-sport aircraft rules. It features a cantilever low-wing, a two-seats-in-side-by-side configuration enclosed cockpit under a bubble canopy, fixed tricycle landing gear and a single engine in tractor configuration.

The aircraft is made from wood. Its 7.30 m (24.0 ft) span wing is rectangular in planform to reduce construction costs. Standard engines available are the 80 hp (60 kW) Rotax 912UL and 80 hp (60 kW) Jabiru 2200. Kit variants for the United States experimental light-sport market use the Rotax 912 and have a gross weight of 600 kg (1,323 lb).

Variants

Pioneer 200 Standard Base model, will accept engines from 60 to 80 hp (45 to 60 kW).

Pioneer 200 Sauer Model powered by a Sauer 1800 UL Volkswagen air-cooled engine.

Pioneer 200 Sparrow Model with luxury interior, carbon fibre instrument panel and Rotax 912ULS engine of 100 hp (75 kW).

Pioneer 200 Beluga Model with extended turtle-deck baggage to carry extended length loads.

Pioneer 230 Model with optional equipment included as standard. Engines available are the 80 hp (60 kW) Rotax 912UL, 100 hp (75 kW) Rotax 912ULS and the 100 hp (75 kW) Rotax 912iS four stroke power plants.

The Pioneer 300 was derived from the Asso V Champion and designed to comply with the Fédération Aéronautique Internationale microlight rules, as well as the US light-sport aircraft rules. It features a cantilever low-wing, a two-seats-in-side-by-side configuration enclosed cockpit under a bubble canopy, a choice of fixed or retractable tricycle landing gear and a single engine in tractor configuration. The fixed landing gear version is intended for the US light-sport aircraft category that does not permit retractable gear on landplanes.

The aircraft is made with a wooden frame, covered with composite skin panels. Its 8.10 m (26.6 ft) span wing is tapered in planform. Standard engines available are the 100 hp (75 kW) Rotax 912ULS, 85 hp (63 kW) Jabiru 2200 and 120 hp (89 kW) Jabiru 3300

Variants

Pioneer 300 Standard

Base model, standard engine is the 100 hp (75 kW) Rotax 912ULS.

Pioneer 300 Hawk

Model with upgraded canopy and interior, with plywood wing skins and oleo strut suspension.

Pioneer 300 Kite

Model with fixed gear and gross weight of 560 kg (1,235 lb) for the US light-sport aircraft market.

Pioneer 300 Turbo

Model with luxury interior, carbon fibre instrument panel and Rotax 914 turbocharged engine of 115 hp (86 kW) giving a cruise speed of 265 km/h (165 mph).

Pioneer 330 Acro

Aerobatic model, with inverted-capable version of the 100 hp (75 kW) Rotax 912ULS and a strengthened airframe with flight load factors of +6/-3g.

Retractable (GA) version

The Alvarez Polliwagen is a 1970s homebuilt aircraft. The aircraft has a combination of many high performance features not typically found in a Volkswagen air-cooled engine-powered homebuilt.

he Polliwagen is a low wing, side-by-side configuration, T tailed, tricycle landing gear equipped aircraft with tip tanks. The aircraft was developed and tested with a one quarter scale radio controlled model. Ailerons and flaps are full span. The fuselage is built from composites with foam cores. The aircraft's engine is configured with a turbocharger and constant speed propeller. Entrance is through a swing up canopy.

In March 1981 Romuald Drlik began the design work for a new lightweight canard-type aircraft, tentativly named Falcon and in May 1981 Romuald and helpers began construction on the first Falcon prototype (model "A"). After first trying a single-wheel gear and side-stick (neither successful) the #1 Falcon flies in late July 1981 using tricycle gear, a double-surface variable camber Dacron wing, centre hinged-stick, and a Robin 240 cc single-cylinder engine.

In August 1983 three pre-production ultralight-legal Falcons were flown at Oshkosh, utilizing Kevlar-and-graphite fuselages and numerous refinements. Two of the planes were delivered to Falcon dealers. One craft won Reserve Grand Champion, then was flown home in one afternoon to Minneapolis (over 260 miles), averaging 57 mph ground speed.

In August 1983, load tests to destruction were performed on the other Oshkosh plane (prototype #9, which was weighed by the EAA at 240 lbs), documenting a load-carrying strength of 7 g's positive, three negative for the main wing and over 10 g positive 5 negative for the forward wing. January 1984 - Deliveries of production Falcons begin.

Wing has swept back leading and trailing edges, and tapering chord; no tail, canard wing. Pitch control by elevator on canard; yaw control by tip-rudders, roll control by full-span ailerons; control inputs through stick for pitch/roll and pedals for yaw. Wing braced from below by struts; wing profile; double-surface. Undercarriage has three wheels in tricycle formation; steel-spring suspension on nosewheel and axle-flex suspension on main wheels. Push-right go-right nosewheel steering connected to yaw control. Brake on nosewheel. Glass-fibre fuselage, partially enclosed. Engine mounted below wing driving pusher propeller.

The Falcon XP two seat tandem verson became available in early 1984.

For more history of the development of the Falcon, click here.

The Eaglet 31 was a United States two-seat tandem ultra-light high-winged monoplane of the early 1930s. Intended as a low-cost aircraft, its limited production run relegated it to a footnote in aviation history.

The American Eagle Aircraft Corporation found that demand for their A-129 biplane and their other models was badly affected by the Wall Street stockmarket crash of late 1929 which ushered in the Great Depression. The small ultra-light, tandem two-seat Eaglet was therefore designed by company president, Edward E. Porterfield, to appeal to pilots with more modest pockets. Porterfield set a realistic goal of manufacturing an aircraft for $1,000. The first advertised price was $995.00.

The first model was the 1930 Eaglet 230, initially powered by the 25 h.p. Cleone engine that flew on June 30, 1930. The engine was so underpowered that only solo flights were possible.

Most later Eaglet 230s featured a 30 h.p. "Zeke" Szekely three-cylinder radial engine. Further experimentation led to fitting a Franklin engine and 60 h.p. Velie. A 40 h.p. Salmson engine was tried but proved to be too expensive to incorporate into the proposed production line. The Szekely eventually ran reliably as an overhead valve 45 h.p. version.

The single Model A-31 of 1931 was fitted with the more powerful Continental A-50 of 50 h.p., and was followed by 13 Model B-31 and B-32 powered by the 45 h.p. Szekely SR-3. The bulk of these examples were produced after the American Eagle company declared bankruptcy and was absorbed by Lincoln Aircraft in May 1931 and reformed as the American Eagle Lincoln Page Aircraft Corporation. The venture was short-lived with the factory closing in 1931.

Production rights to the Eaglet later went to American Eaglecraft who produced three examples from 1940–1947 and rebuilt further aircraft of this design.

Variants

Eaglet 230  (Specifications below)
30 h.p. Szekely SR-3;
Eaglet 231
40 h.p. Salmson AD-9 (2 modified from model 230);
Eaglet A-31
50 h.p. Continental A-50;
Eaglet B-31 & B-32
45 h.p. Szekely SR-3; (B-32 had minor control modifications)

The American Legend AL3C-100 and American Legend AL11C-100 are new design American light-sport aircraft inspired by the Piper J-3 Cub and Super Cub.

The Legend Cub is built closely along the lines of the original Piper Cub with modern materials, engines and instruments. The aircraft is a high-wing, tandem seat monoplane with conventional landing gear. The fuselage is constructed with welded steel tubing with doped Superflite aircraft fabric.

In April 2015 the Super Legend design was further developed with the addition of a greater number of carbon fibre components, including doors, floorboards, the propeller spinner and the wingtip bows. Avionic upgrades include Garmin G3X avionics and a FreeFlight Systems 1201 WAAS GPS sensor, Trig Mode S and 1090ES ADS-B Out transponder.

Variants

Diesel Engine
In July 2015, American Legend Aircraft and Superior Air Parts (makers of the Gemini engine) announced that the 100-horsepower Gemini turbo-charged diesel engine would be available in 2016 as an option throughout the American Legend product line. The engine burns widely available Jet A and/or diesel fuel; an important consideration as normal aviation 100LL gasoline is expensive or unavailable in many remote areas. Power, price and weight are said to be comparable to the existing Continental O-200 avgas engine, but with a 20% lower fuel burn.
AL11C-100
Designed to resemble a Piper PA-11 Cub Special with an enclosed cowling.
AL3C-100   (Specifications below)
Designed to resemble a Piper J-3 Cub with cylinders exposed through the cowling.
AL11J-120
Powered with a 120 hp (89 kW) Jabiru 3300 engine.

AL18 Super Legend
Lycoming IO-233 powered variant designed to resemble a Piper PA-18 Super Cub. Kevlar and carbon fiber floats certified for aircraft in 2015. 2015 Super Legend re-engined with Lycoming YO-233 115hp variant accepting 100LL AvGas and Automotive Fuel.

MOAC
The Mother of all Cubs model is a modification of the AL18 for back country flying and off-airport operations, with shock absorbing landing gear and a Continental Titan O-340 engine of 180 hp (134 kW). Introduced in July 2020, it features large flaps that deploy to 40°, leading-edge slats and square wingtips all intended to improve low-speed handling. The variant is available as a light-sport aircraft or homebuilt aircraft kit.[9]
Texas Sport Cub
Homebuilt kit.

The American Legend AL3C-100 and American Legend AL11C-100 are new design American light-sport aircraft inspired by the Piper J-3 Cub and Super Cub.

The Legend Cub is built closely along the lines of the original Piper Cub with modern materials, engines and instruments. The aircraft is a high-wing, tandem seat monoplane with conventional landing gear. The fuselage is constructed with welded steel tubing with doped Superflite aircraft fabric.

In April 2015 the Super Legend design was further developed with the addition of a greater number of carbon fibre components, including doors, floorboards, the propeller spinner and the wingtip bows. Avionic upgrades include Garmin G3X avionics and a FreeFlight Systems 1201 WAAS GPS sensor, Trig Mode S and 1090ES ADS-B Out transponder.

Variants

Diesel Engine
In July of 2015, American Legend Aircraft and Superior Air Parts (makers of the Gemini engine) announced that the 100-horsepower Gemini turbo-charged diesel engine would be available in 2016 as an option throughout the American Legend product line. The engine burns widely available Jet A and/or diesel fuel; an important consideration as normal aviation 100LL gasoline is expensive or unavailable in many remote areas. Power, price and weight are said to be comparable to the existing Continental O-200 avgas engine, but with a 20% lower fuel burn.
AL11C-100
Designed to resemble a Piper PA-11 Cub Special with an enclosed cowling.
AL3C-100
Designed to resemble a Piper J-3 Cub with cylinders exposed through the cowling.
AL11J-120
Powered with a 120 hp (89 kW) Jabiru 3300 engine.

AL18 Super Legend
Lycoming IO-233 powered variant designed to resemble a Piper PA-18 Super Cub. Kevlar and carbon fiber floats certified for aircraft in 2015. 2015 Super Legend re-engined with Lycoming YO-233 115hp variant accepting 100LL AvGas and Automotive Fuel.

MOAC
The Mother of all Cubs model is a modification of the AL18 for back country flying and off-airport operations, with shock absorbing landing gear and a Continental Titan O-340 engine of 180 hp (134 kW). Introduced in July 2020, it features large flaps that deploy to 40°, leading-edge slats and square wingtips all intended to improve low-speed handling. The variant is available as a light-sport aircraft or homebuilt aircraft kit.
Texas Sport Cub
Homebuilt kit.

AL18 Super Legend

The AMF Chevvron is a British two-seat microlight aircraft of the 1980s and 90s. It is a single engined mid-winged monoplane with side-by-side seating. 41 were built.

The Chevvron was designed to meet a requirement for an aircraft conforming with the Civil Aviation Authority's regulations for microlight aircraft and fitted with conventional three-axis controls. The Chevvron is a mid-wing monoplane with a pod-and boom configuration and high aspect ratio wings. It is built of composite materials and is fitted with a fixed nosewheel undercarriage. The normal powerplant was a single König SD 570 two-stroke, four-cylinder air-cooled radial engine rated at 32 horsepower (24 kW) and driving a three-bladed propeller.

The first prototype, fitted with a V-tail, made its maiden flight in late 1983. A modified second prototype, with a conventional tail flew in October 1986.

AMF Microflight began production of the Chevvron in 1987, with 19 completed at their Membury factory by 1990. A single example was built of the Sea Chevvron, a floatplane version fitted with a more powerful (48 horsepower (36 kW)) König engine, while examples were also fitted with a 45 horsepower (34 kW) Limbach engine. In total, 41 Chevvrons were built. In the 1990s, as single-rotor wankel engine from the MidWest AE series was successfully fitted to a Chevvron.

The Anderson EA-1 Kingfisher is a US two-seat amphibious aircraft designed and marketed for homebuilding.

It was the work of Earl William Anderson, a Pan Am airline captain, who flew the prototype on 24 April 1969. By 1978, 200 sets of kits for the plane had been sold, and 100 Kingfishers were reported to be under construction. The aircraft is a shoulder-wing monoplane with a flying boat hull and outrigger pontoons. On land, it uses retractable tailwheel undercarriage. The single engine with a tractor propeller is mounted in a nacelle above the wing. Some builders utilize the wings from a Piper Cub rather than making their own.

The planes were later marketed by Richard Warner Aviation before becoming the Wings Unlimited Kingfisher in the late 1990s. A variant with improved performance is known as the 'Super Kingfisher'.

The Andreasson BA-4B is a single-seat aerobatic biplane which was marketed for homebuilding and also produced complete.

The BA-B4B was based on Andreasson's 1944 wooden BA-4 revised to take advantage of more modern construction techniques, such as the use of sheet metal. The first example was built by apprentices at the Malmö Aircraft Industry (M.F.I.). It is a single-bay, staggered-wing biplane with fixed tailwheel undercarriage. P.J.C Phillips acquired worldwide production rights for complete, rather than kit built, version and marketed them in the UK through Crosby Aviation. In the US the B-4B was marketed by Larry Karp as the Canary Hawk.

In 2014 there were six BA-4Bs on the UK civil register, one Crosby built and the others homebuilt. Three of these have the Continental O-200-A engine but the other three use Lycoming flat fours with outputs between 81 kW (108 hp) and 119 kW (160 hp). In 2009 four BA-4Bs remained on the Swedish register.

Variants

Andeasson B-4 (Midget)
Wood and fabric biplane first flown in 1944, powered by a 21 kW (28 hp) Scott Squirrel.
Andreasson B-4B
All-metal version. First prototype built by M.F.I apprentices in c.1964. Plans marketed.
Crosby (Andreasson) B-4B
Sold complete, powered by a 75 kW (100 hp) Rolls-Royce Continental O-200-A flat four.
Crosby (Andreasson) Super B-4B
As B-4B but with a 89 kW (120 hp) Rolls-Royce Continental O-240-A flat four.