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Littner Whiskey IV

Asso Aerei Whiskey IV


litwhis4


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

 

 

 


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