Lloyd C.V
1 engine
Lloyd C-II
Lloyd B-VI
Lloyd Liberty Sport A
An original design of O.N. Lloyd, a 47 yr old construction engineer of Mesa, Arizona, USA, the two-seat Liberty Sport A, registered N185L, has wing with spruce spars and metal ribs. The fuselage and tail surfaces are 4130 tubing, and Ceconite covering is used throughout. Ailerons are fitted to the top wing only.
Cost of construction was about $4000 over four years.
Engine: Lycoming O-320, 150 hp
Wingspan: 28 ft / 8.53 m
Length: 22 ft 4 in / 8.81 m
Height: 8 ft / 2.44 m
Wing chord: 4 ft / 1.22 m
Empty weight: 1325 lb / 601 kg
MAUW: 2000 lb / 907 kg
Max speed: 120 mph / 193 kph
Cruise: 105 mph / 169 kph
Landing speed: 50 mph / 80 kph
ROC: 900 fpm / 4.58 m/sec
TO to 50 ft / 15.2m: 1000 ft / 304 m
Service ceiling: 15,000 ft / 4572 m
Range: 375 mi / 604 km
LJaM 1912 Monoplane
Jerzy Jankowski, Maximilian von Lerche and Francesco Mosca built at workshops of Moscov Aeronautical Society and airplane modeled after Bleriot aircraft with 50hp Gnome engine. It was apparently very well designed and built aircraft that made numerous succesful flights, including one on 14th of May 1912 when Jankowski broke on it Russian flight altitude record of 1775m;
Liwentaal Libellule
The first Swiss airplane to leave the ground, a tandem-wing monoplane designed by the Estonian-born inventor Alexandre Liwentaal of Vernier, near Geneva, Switzerland. It was tested in September 1909, but it was underpowered and only managed jumps of 25 meters.
Wing surface: 29 sq.yards
Weight all up: 551 lbs
Littner Whiskey IV / Asso Aerei Whiskey IV
The Whisky IV is a tandem two seat, low wing aircraft designed by Giuseppe Vidor. Construction materials are wood & fabric. The landing gear is a fixed tailwheel configuration.
2009 Complete set of plans $400 (US$)
Engine: Limbach 2000, 80 hp
HP range: 75-100
Wing Span: 26.25 ft.
Wing Area: 120.5 sq. ft.
Length: 21 ft.
Height: 7 ft.
Cockpit Width: 28.3 in.
Aspect Ratio: 5.7
Dihedral Angle: 4°
Wash Out: 1.50°
Empty Weight: 622 lbs.
Gross Weight: 1058 lbs.
Wing Loading: 8.78 lbs./sq. ft.
Power Loading: 13.22 lbs./HP
C.G. Travel: 18.3 to 31% MAC
Fuel Capacity: 13.2 gal. / 79 lbs.
V.N.E: 175 mph.
Max Horizontal Speed: 160 mph.
Cruise 75% Power: 130 mph.
Max Maneuvering Speed: 115 mph.
Max Flap Speed: 84 mph.
Stall Speed Flaps Down: 37 mph.
Stall Speed Flaps Up: 43 mph.
Take-Off Distance: (Solo) 330 ft.
Landing Distance: (Solo) 490 ft.
Fuel Burn 75% Power: 3.17 gal./hr.
Max Range 75% Power: 535 nm
Rate Of Climb: 785 ft./min.
Service ceiling: 12,000 ft
Seats: 2 tandem
Landing gear: retractable tailwheel
Littner Supercab
A low tapered wing equipped with slotted flaps and retractable tailwheel undercarriage.
Top speed: 162 mph
Cruise: 143 mph
Stall: 35 mph
Range: 500 nm
Rate of climb: 960 fpm
Takeoff dist: 330 ft
Landing dist: 330 ft
Service ceiling: 12,000 ft
Engine: Continental C-90, 90 hp
HP range: 65-110
Fuel capacity: 17 USG
Empty weight: 750 lb
Gross weight: 1250 lb
Height: 5.5 ft
Length: 18 ft
Wing span: 27 ft
Wing area: 111 sq.ft
Seats: 2
Landing gear: retractable tailwheel
Littner Champion V / Asso Aerei Champion V / Vidor Guiseppe Asso V
The Champion V is a side by side two seat, low wing aircraft designed by Giuseppe Vidor. Construction materials are wood & fabric. And the landing gear can be built in fixed trigear or retractable trigear configurations.
2009 Complete set of plans $400 (US$)
The Asso V Champion was built by Alpi Aviation with composite skin panels as the Pioneer 300.
Undercarriage: Fixed
Engine: Limbach 2000, 80 hp
Wing Span 27.3 ft.
Wing Area 120 sq. ft.
Length 20 ft.
Gross Weight 993 lbs.
Fuel 78 lbs.
G Loads (Ultimate) +5.7, -2.67
Horsepower Range 75 to 100
Empty Weight: 595 to 604 lbs.
Max Speed: 130 mph.
Cruise 75% Power: 107 mph.
Cruise 90% Power: 115 mph.
Stall Speed: 40 mph.
V.N.E: 160 mph.
R.O.C: 800 ft./min.
Take-Off Distance: 425 ft.
Landing Distance: 330 ft.
Range: 425 miles
Maneuvering Speed: 95 miles
Max Speed With Flaps: 70 mph.
Undercarriage: Retractable
Engine: Limbach 2000, 80 hp
Wing Span 27.3 ft.
Wing span: 27.3 ft
Wing Area 120 sq. ft.
Length: 20 ft.
Height: 7 ft
Gross Weight 1058 lbs.
Fuel 13 USG / 78 lbs.
G Loads (Ultimate) +5.7, -2.67
Horsepower Range 75 to 100
Empty Weight 617 lbs.
Max Speed: 140 mph
Cruise 75% Power: 103 kt / 118 mph / 190 kmh
Cruise 90% Power: 127 mph.
Stall Speed: 34 kt / 39 mph / 63 kmh
V.N.E: 139 kt / 160 mph / 258 kmh
R.O.C: 800 ft/min / 4 m/s
Take-Off Distance: 425 ft.
Landing Distance: 330 ft.
Range: 425 miles
Maneuvering Speed: 105 miles
Max Speed With Flaps: 70 mph.
Service ceiling: 12,000 ft
Seats: 2
2009 Price: 66000 EURO
Vidor Guiseppe Asso V
Engine: Rotax 912, 80 hp
Wing span: 8.3 m
Wing area: 11 sq.m
MAUW: 450 kg
Empty weight: 275 kg
Fuel capacity: 55 lt
Max speed: 245 kph
Cruise speed: 225 kph
Minimum speed: 62 kph
Climb rate: 4.5 m/s
Seats: 2
Fuel consumption: 13 lt/hr
Plan price (1998): 800 000 L
Kit price (1998): 12 172 000 L
Littner Junior IV / Asso Junior / Asso Aerei Junior IV / Asso Junior / Vidor Guiseppe Asso IV Wisky
A wood and fabric design by Giuseppe Vidor. The side by side two seater is capable of modest aerobatics.
Top speed: 125 mph
Cruise: 100 mph
Stall: 38 mph
Range: 375 nm
Rate of climb: 600 fpm
Takeoff dist: 350 ft
Landing dist: 400 ft
Service ceiling: 10,000 ft
Engine: Limbach, 62 hp
HP range: 50-65
Fuel capacity: 15 USG
Empty weight: 530 lb
Gross weight: 950 lb
Height: 5.9 ft
Length: 20 ft
Wing span: 28.6 ft
Wing area: 123.7 sq.ft
Seats: 2
Landing gear: retractable nose wheel
Vidor Guiseppe Asso IV Wisky
Engine: Sterpha, 85 hp
Wing span: 8.1 m
Wing area: 11.2 sq.m
MAUW: 450 kg
Empty weight: 285 kg
Fuel capacity: 50 lt
Max speed: 245 kph
Cruise speed: 225 kph
Minimum speed: 63 kph
Climb rate: 5 m/s
Seats: 2
Fuel consumption: 12 lt/hr
Plan price (1998): $450
Kit price (1998): 15 000 000 L
