LSA legal
Cruise: 103 mph
Stall: 42 mph
Range: 645 sm
Rate of climb: 1200 fpm
Takeoff dist: 600 ft
Landing dist: 500 ft
Engine: Jabiru, 80 hp
HP range: 80-150
Fuel capacity: 20 USG
Empty weight: 618 lb
Gross weight: 990 lb
Length: 18.3 ft
Wing span: 26 ft
Wing area: 80 sq.ft
Cockpit width: 44 in
Landing gear: nose wheel
The US agent for plans and kits was Micro Technologies Inc.
Top speed: 220 mph
Cruise: 165 mph
Stall: 60 mph
Range: 600 nm
Rate of climb: 1000 fpm
Takeoff dist: 1300 ft
Landing dist: 500 ft
Service ceiling: 14,000 ft
Engine: Lycoming O-320, 150 hp
HP range: 150-180
Fuel capacity: 50 USG
Empty weight: 1000 lb
Gross weight: 1600 lb
Height: 5 ft
Length: 18 ft
Wing span: 26 ft
Wing area: 90 sq.ft
Seats: 2
Landing gear: nose
Designed in 1988, the retractable L7 can fit up to 200 hp without modification. The 5 x 4 ft door permits large item loading, or parachute dropping.
Top speed: 142 mph
Cruise: 110 mph
Stall: 44 mph
Range: 560 nm
Rate of climb: 500 fpm
Takeoff dist: 1540 ft
Landing dist: 1700 ft
Service ceiling: 13,00 ft
Engine: Lycoming O-235, 115 hp
HP range: 115-180
Fuel capacity: 30 USG
Empty weight: 1150 lb
Gross weight: 1750 lb
Height: 8 ft
Length: 21 ft
Wing span: 34 ft
Wing area: 133 sq.ft
Seats: 2
Landing gear: nose or tail wheel/retractable
A motorglider with either nose or tail wheel. It can be flown with a 28 ft wing and O-235 engine. A removable wing extension was optional. The wings fold and detach.
The US agent for plans and kits was Micro Technologies Inc.
Top speed: 110 mph
Cruise: 98 mph
Stall: 44 mph
Range: 621 nm
Rate of climb: 450 fpm
Takeoff dist: 1480 ft
Landing dist: 1600 ft
Service ceiling: 14,000 ft
Engine: Limbach, 80 hp
Fuel capacity: 20 USG
Empty weight: 990 lb
Gross weight: 1480 lb
Height: 8 ft
Length: 22 ft
Wing span: 15 ft
Wing area: 180 sq.ft
Seats: 2
Landing gear: nose or tail wheel
Engine: Lycoming O-235
Wing span: 9 m
Wing area: 13 sq.m
MAUW: 750 kg
Empty weight: 490 kg
Fuel capacity: 150 lt
Max speed: 260 kph
Cruise speed: 230 kph
Minimum speed: 100 kph
Climb rate: 3 m/s
Seats: 2
Fuel consumption: 28 lt/hr
Plan price (1998): 2500 Fttc
Designed as a 2, 3, or 4 place with and identical airframe. Was available as either nose or tail wheel.
The US agent for plans and kits was Micro Technologies Inc.
Top speed: 165 mph
Cruise: 118 mph
Stall: 54 mph
Range: 620 nm
Rate of climb: 520 fpm
Takeoff dist: 1450 ft
Landing dist: 1600 ft
Service ceiling: 13,000 ft
Engine: Lycoming O-320, 150 hp
HP range: 108-180
Fuel capacity: 50 USG
Empty weight: 1150 lb
Gross weight: 1900 lb
Height: 6 ft
Length: 20 ft
Wing span: 31 ft
Wing area: 133 sq.ft
Seats: 2-4
Landing gear: nose
A 75% scale replica of Sopwith Camel F9509 designed and built by John Lowther.
Engine: Webster 5-cyl radial.
Built by C.H Lowe-Wylde in 1932, the Planette was a B.A.C. VII glider modified to a single seater with an engine fitted on top of the wing.
Built by F.H. Lowe, in 1920 in Newcastle, UK, the Lowe HL(M)9 Marlburian was a two-place side-by-side braced monoplane, powered with a Gnome rotary engine. It was registered G-EBEX s/n HL(M)9, first flying in 1921.
It was written off on 25 November 1922.
Engine: Gnome
Wing span: 22.06 ft
Length: 17.00 ft
Built by the Lovington brothers Ted, Joseph, Leon and Joe, on Staren Island, NY., USA.
No information on its success.
The Love racer features reverse-gull wings and full wheel covers. It is built from fabric around a wood frame. With an 85-hp Continental powerplant, it is capable of speeds in ex¬cess of 200 mph.
Engine: 85-hp Continental
Gross Wt. 885 lb
Empty Wt. 613 lb
Fuel capacity 15 USG
Wingspan 20 ft
Length 17 ft 2 in
Top speed: 215 mph.
Cruise 142 mph.
Stall 58 mph.
Climb rate 2100 fpm
Takeoff run 500 ft.
Landing roll 1200 ft
Range 450 miles
