The Macro is an all metal low wing monoplane. The cantilever wind consists of a built up “I” beam spar with hand beaten aluminium ribs. The monocoque fuselage is of 2024T3 aluminium. A twin seat version was under construction which will have twin wing mounted engines.
Engine: Fuji Robin 244.
Prop: 81 cm x 38 cm pitch.
Wingspan: 7.0m.
Length: 3.96m.
Weight: 89.8 kg.
Fuel capacity: 18 ltr.
Econ cruise speed: 56 kts.
Stall: 35kts.
1985: Elite Aircraft. 2 Yardley Drive, Mulgrave Vic 3170. Australia.
LSA builder
The Sigma 4 was designed for training, tourism and sport.
The airplane was designed according to requirements of JAR VLA
Engine: Rotax 912 ULS
Power: 100 hp
Take-off weight: 544 kg
Emty weight: 360 kg
Max speed: 115 knts
Cruise speed: 90 knts
Minimal speed: 30 knts
Rate of climb: 8 m/s
Take off distance(nil wind): 70 m
Landing distance (nil wind): 100 m
Range: 700km
Perfomance overload: +4-1
Flaps: electric
A single seat enclosed helicopter that was originated by Augusto Cicare in 1973. Welded 4130 steel tube frame with composite enclosure. Tail boom and skids are of aluminium alloy. Manufactured in Turin, Italy.
The flight qualities were improved by fitting 8 H 12 blades. It can be powered by a Rotax 912.
Engine: Rotax 582, 64 hp
Rotor span: 6.5 m
Blade area: 0.18 sq.m
MAUW: 360 kg
Empty weight: 205 kg
Fuel capacity: 40 lt
Max speed: 140 kph
Cruise speed: 136 kph
Minimum speed: 0 kph
Climb rate: 10 m/s
Seats: 1
Fuel consumption: 13 lt/hr
CH-7
Engine: 65 hp Rotax 582.
Rotor blades: Composite 19 ft
Metal tail rotor: 40 in
Speed max: 86 mph.
Cruise: 68 mph.
Range: 205 sm.
ROC: 1200 fpm.
Service ceiling: 11,000 ft.
Fuel cap: 10 USG.
Weight empty: 374 lbs.
Gross: 682 lbs.
Height: 6.75 ft.
Length: 23 ft.
Disk span: 19 ft.
Landing gear: skids.
Seats: 1
Engine: 80 hp Rotax 582.
Rotor blades: Composite 19 ft
Metal tail rotor: 40 in
Speed max: 100 mph.
Cruise: 80 mph.
Range: 170 sm.
ROC: 1900 fpm.
Service ceiling: 11,000 ft.
Fuel cap: 10 USG.
Weight empty: 451 lbs.
Gross: 792 lbs.
Height: 6.75 ft.
Length: 23 ft.
Disk span: 19 ft.
Landing gear: skids.
Seats: 1
The prototype CH-6 was created in 1987 and evolved into the CH-7.
1997: St.da Traforo del Pino 102
10132 TORINO Italy
UL helicopter builder
In 2008 was the debut of the ElectraFlyer-C at the Experimental Aircraft Association AirVenture in Oshkosh. This all-electric, single passenger aircraft, fitted with a custom-built lithium polymer battery pack was able to cruise at 70 mile/h for 1–1/2 to 2 h and charged in as little as 2 hours.
The ElectraFlyer-C was designed and built as a prototype and proof of concept for economical electric flight.
Elam Eurocub has larger tail fin and elevator than the older Cuby and that gives a lower stall speed.
Stall: 32 kt / 37 mph / 59 kmh
Cruise: 85 kt / 98 mph / 157 kmh
VNE: 110 kt / 127 mph / 204 kmh
Empty Weight: 269 kg / 593 lbs
MTOW Weight: 450 kg / 992 lbs
Climb Ratio: 1200 ft/min / 6 m/s
Glide Ratio: 1:11
Take-off distance (50ft obstacle): 330 ft / 100 m
Landing distance (50ft obstacle): 330 ft / 100 m
Stall: 35 kt / 40 mph / 65 kmh
Cruise: 86 kt / 99 mph / 160 kmh
VNE: 97 kt / 112 mph / 180 kmh
Empty Weight: 280 kg / 617 lbs
MTOW Weight: 480 kg / 1058 lbs
Climb Ratio: 1200 ft/min / 6 m/s
Take-off distance (50ft obstacle): 330 ft / 100 m
Landing distance (50ft obstacle): 490 ft / 150 m
2009 Price: 35000 EURO
All Aero 