BUILD ULTRALIGHT QUICKIE Q1 Q2 Q200 AIRPLANE PLANS PLUS EXTRAS ON DVD

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QUICKIE Q1 Q2 Q200<br>quickie plans<br>This auction is for a CD loaded with information about   a radical  aircraft the 'Quickie'.<br>The Quickie is a single-seat light aircraft of canard  configuration.   built of foam core is extremely light. This plane made  all the requirements   for ultralight designation; except for, speed!  It's too fast! Thus the name   'Quickie'.<br>You get blueprints. Software on building   your own  propellers, wind tunnel, airfoils... Quickie Templates.<br>Fligh Simulator Sequence.<br>Try it before you build!<br>Plus videos of flight tests. Find out why they call it a quickie!<br>Partial list  of contents:<br>Quickie Plans, Quickie Parts List, Q2 Plans, Q200 Plans Section II, Q2 LS1 Canard Templates, Q2 Belly Board, Q2 Front Hinged Canopy.<br>Q2 Hydraulic Brakes, Q2 Pilot Operating Handbook, Q2 Reflexor, Q200 LS1 Construction ,Q2 Pilot    Manual<br>Q200 Pilot Operating Handbook  Supplement.   Also details on  Subaru atomobile  engine conversion. And much more...<br>Quickie<br>Type:<br>Single-seat light sporting aircraft of canard configuration.<br>Wings:<br>Tapered cantilever shoulder-wing monoplane. Dihedral    from roots. Two unidirectional glassfiber spars and shaped low-density rigid    foam core, covered with glassfiber. Constant cord inboard ailerons. No flaps.<br>Foreplane:<br>Tapered and slightly sweptback cantilever foreplane,    mounted low on forward fuselage. Marked anhedral. Construction similar to    that of wings. Main-wheel housings attached to tips. Full span tapered elevator/flaps.<br>Fuselage:<br>Semi-monocoque structure of banana shape, formed    from 25 mm (1 inch) thick foam, with glassfiber covering inside and out,   and tapered towards rear. Foam/glassfiber sandwich bulkheads.<br>Tail Unit:<br>Cantilever sweptback vertical fin and narrow chord    of similar construction to wings.<br>Landing Gear:<br>Non-retractable tailwheel type. Main-wheels positioned    at tips of foreplane in swept fairings. A kit to provide 50% larger types    for grass field operations is optional. Steerable tailwheel and the fuselage.<br>Power Plant:<br>One modified Onan horizontally opposed two-cylinder    four-stroke engine, developing originally 13.5 kW (18 hp) at 3,600 rpm and    driving a two-blade fix-pitch wooden propeller. Modifications to cylinder    heads and exhaust system allowed newly supplied engines to developed 16.4    kW (22 hp) at 3,800 rpm: a retrofit kit is available to convert 13.5 kW (18   hp) engines to develop this increased output. Fuel capacity 30.3 liters (8   US gallons). Fuel consumption approximately 44.2 km/liter (104 mi/US gallon).<br>Accommodation:<br>Single seat under one-piece side-hinged canopy. Cockpit suitable for pilot up to 1.98 m (6 ft 6 in) tall and weighing up to 95 kg (210 lb). Max baggage capacity with lighter pilot 13.6 kg (30 lb). With the engine developing 16.4 kW (22 hp), a 100 kg (220 lb) pilot, maximum fuel, and 5.4 kg (12 lb) of baggage can be carried.<br>Dimensions, External<br>Wing span:<br>5.08 m (16 ft 8 in)<br>Foreplane span:<br>4.67 m (15 ft 4 in)<br>Length overall:<br>5.28 m (17 ft 4 in)<br>Dimensions, Internal<br>Cockpit, Length:<br>1.63 m (5 ft 4 in)<br>Cockpit, width:<br>0.56 m (1 ft 10 in)<br>Cockpit, height:<br>0.86 m (2 ft 10 in)<br>Areas<br>Wings, gross:<br>2.52 m² (27.08 ft.²)<br>Foreplane, gross:<br>2.47 m² (26.57 ft.²)<br>Weights<br>A = 13.5 kW (18 hp) Engine<br>B = 16.4 kW (22 hp) Engine<br>Weight, empty:<br>A: 109 kg (240 lb)<br>B: 109 kg (240 lb)<br>Max T-O weight:<br>A: 218 kg (480 lb)<br>B: 236 kg (520 lb)<br>Performance<br>Max level speed:<br>A: 109 knots (202 km/h; 126 mph)<br>B: 122 knots (225 km/h; 140 mph)<br>Max cruising speed:<br>A: 105 knots (195 km/h; 121 mph)<br>B: 115 knots (214 km/h; 133 mph)<br>Stalling speed, power off:<br>A: 46 knots (86 km/h; 53 mph)<br>Stalling speed, power on:<br>A: 43 knots (79 km/h; 49 mph)<br>Normal rate of climb at S/L:<br>A: 130 mpm (425 fpm)<br>B: 183 mpm (600 fpm