Aviaimpex Yanhol / Angel

With the prototype structurally complete, the Aviaimpex Yanhol was displayed to the media on 31 August 2001. First flight was planned for June 2002.
Of pod-and-boom configuration, with T-tail and landing skids, the three seat helicopter has three-blade main and two-blade tail rotors.
COSTS: US$120.000 in Ukraine; US$150.000 export (2002),

Enghines: Two Rotax 912 ULS, 73.5kW.
Main rotor diameter: 8.28m
Tail rotor diameter: 1.30m
Length: 7.45m
Height: 2.475m
Max. take-off weight: 870kg
Empty weight: 524kg
Max. payload: 350kg
Max. speed: 184km/h
Max. cruising speed: 165km/h
Range max. fuel: 340km

Avia Baltika Aviation Ltd

Incorporated 1991 and founded from the Kaunas helicopter service and repair factory, markets in assembled and kit forms the two-seat composites LAK-X lightplane (first flown 1992 and developed by Aeroplastika). Other work includes overhaul of helicopters and aviation equipment/components, aircraft leasing, transport operations, and rescue work using company-owned Mil helicopters.

AVIC Special Vehicle Research Institute A2C

AC2-L

The A2C-L ultra-light aircraft was developed by the AVIC Special Vehicle Research Institute after the A2C seaplane achieved commercial success. The aircraft is transformed and updated from the seaplane and finished its test flight in 2012.

The A2C seaplane is the first ultra-light aircraft that obtained a certificate of model design approval and a production permit issued by the Civil Aviation Administration of China.

An ultra-light aircraft independently developed by China, it got the special flight permit and completed its delivery test flight on 11 March 2016. Nearly 100 A2C planes have been sold to regions including Sichuan, Hubei, Anhui, Inner Mongolia and Xinjiang.

AVIAD Zigolo MG12

The AVIAD Zigolo MG12 is a SSDR (Single Seat De-Regulated) ultralight motor glider. This aircraft meets the USA FAA FAR Part 103 rules for UL (SSDR) aircraft in USA, China, and other countries. It is a conventional full 3-axis aircraft.

The AVIAD Zigolo MG12 is specifically designed for simple construction and low cost of ownership, it has a traditional tubular frame structure and simple bonded fabric covering. It has excellent slow flight characteristics and a short landing and take off distance of 130 feet.

The rear mounted pusher engine with propeller and the fuel tank are also contained within the airframe. The joy stick mounted engine throttle control further simplifies the aircraft’s three axis flight controls. It incorporates a forward pilot cockpit protected by the fuselage frame work and providing a wide field of view.

The Zigolo MG12 Kit does not require specialist knowledge or equipment for assembly. The drawings are very detailed and provide a step by step guide for assembly. The individual drawings contain a parts list of required components, which are easily identified by the initials engraved on them.

The Design Drawings are shared online and are made easily accessible for kit builders. All parts are accurately cut, perforated and folded. The assembly process only requires the correct part selection and correct positioning prior to fixing with either bolt or rivet to complete each sub-assembly / module. The complete aircraft’s final assembly can be undertaken either within the workshop or in the hangar and does not require any excessive space for construction.

The Zigolo MG12 kit requires less than 100 hours for assembly. The aircraft modules once completed can be rigged and ready to fly in 1 hour and offer easy transportation by truck, pick-up or trailer. The new wing remove system means the wings can be removed in just a couple minutes each.

It is a motor-glider. The glide ratio (L/D) is nowhere near that of a glider but due to its’ large wing and therefore very low wing loading the sink rate is reasonably low. The turn radius is so tight and slow it is easy for novice glider pilots to stay in thermals.

The Zigolo is available as a finished aircraft. Ultralights do not have any 51% build rule like the experimental class but can be offered ready to fly. Should a builder choose to fly outside the Part 103 rules the Zigolo has been inspected and approved as an E-AB kit and can be found on the FAA list of approved kits.

Base price was $12,000 (2017) and that includes EVERYTHING but finish paint. Engine & prop as well.

Engine: Vittorazi Moster 185, 25 hp at 7800 rpm
Wingspan: 11.1m / 36.4 ft
Wingarea: 15.8 sq.m / 170 sq.ft
Length: 5.5 m / 18 ft
Aspect ratio: 7.9
Dihedral: 3 deg
Empty weight: 102 kg / 225 lb
Max weight: 220 kg / 485 lb
Fuel burn: 6 lt/hr / 1.6 GPH
Fuel burn 30kg thrust: 3.5 lt/hr / 0.92 GPH
Stall: 35 kph / 22 mph
Cruise 6800 rpm: 68 kph / 42 mph
Vne: 95 kph / 58 mph
ROC: 2 m/s / 394 fpm
Sink rate: 1.4 m/s / 276 fpm
Glide ratio: 11-1
Manoeuvring speed: 65 kph / 40 mph
Range: 95 km / 59 miles
Load factor: +4 / -2 G
Safety factor: 1.5 G
Tailplan span: 3 m / 9.8 ft
Height at rudder: 1.3 m / 4.3 ft
Power loading: 7 kg/hp 15.4 lb/hp
Wing loading: 11 kg/sq.m / 2.23 lb/sq.ft
TO dist: 40m / 131 ft
TO dist to 50ft: 180m / 590 ft

Australian Aviation Works Spacewalker

Spacewalker I
Spacewalker II

Spacewalker I
Engine: 105 hp.
HP range: 65-105.
Speed max: 140 mph.
Cruise: 120 mph.
Range: 300 sm.
Stall: 38 mph.
ROC: 950 fpm.
Take-off dist: 300 ft.
Landing dist: 250 ft.
Service ceiling: 10,000 ft.
Fuel cap: 10 USG.
Weight empty: 540 lbs.
Gross: 850 lbs.
Height: 5.41 ft.
Length: 17.25 ft.
Wing span: 26 ft.
Wing area: 117 sq.ft.
Seats: 1.
Landing gear: tail wheel.

Spacewalker II
Engine: 108 hp.
HP range: 85-125.
Speed max: 125 mph.
Cruise: 115 mph.
Range: 350 sm.
Stall: 42 mph.
ROC: 950 fpm.
Take-off dist: 300 ft.
Landing dist: 250 ft.
Service ceiling: 10,000 ft.
Fuel cap: 18 USG.
Weight empty: 700 lbs.
Gross: 1200 lbs.
Height: 5.41 ft.
Length: 19.75 ft.
Wing span: 28 ft.
Wing area: 126 sq.ft.
Seats: 2.
Landing gear: tail wheel.

Australian Aviation Works Aerilite 1+1

A single-seat cabin monoplane in plans or kit forms. Maximum engine weight of 210 lbs.

Engine: 75 hp.
HP range: 50-100.
Speed max: 100 mph.
Cruise: 75 mph.
Range: 240 sm.
Stall: 31 mph.
ROC: 900 fpm.
Take-off dist: 300 ft.
Landing dist: 200 ft.
Service ceiling: 10,000 ft.
Fuel cap: 10 USG.
Weight empty: 350 lbs.
Gross: 680 lbs.
Height: 5.83 ft.
Length: 17.5 ft.
Wing span: 30 ft.
Wing area: 120 sq.ft.
Seats: 1.
Landing gear: tail wheel.