The Ultimate 10-200 is a Canadian homebuiltaerobaticbiplane that was designed produced by Streamline Welding of Hamilton, Ontario, introduced in the 1990s. When it was available the aircraft was supplied as a kit or in the form of plans for amateur construction.[1]
The aircraft is made from metal with its flying surfaces covered in dopedaircraft fabric. Its wing span is only 16.00 ft (4.9 m). The acceptable power range varies by each model. Standard equipment includes an inverted fuel system and rear-hinged canopy. Operational g loads are +7 and -5 g. The aircraft has a roll rate of 360 degrees per second.[1]
The 10-200 version has a typical empty weight of 925 lb (420 kg) and a gross weight of 1,320 lb (600 kg), giving a useful load of 395 lb (179 kg). With full fuel of 22 U.S. gallons (83 L; 18 imp gal) the payload for the pilot and baggage is 263 lb (119 kg).[1]
The standard day, sea level, no wind, take off with a 200 hp (149 kW) engine is 450 ft (137 m) and the landing roll is 500 ft (152 m).[1]
The manufacturer estimated the construction time from the supplied kit as 1200 hours.[1]
^Transport Canada (15 March 2014). . Archived from the original on 18 July 2011. Retrieved 15 March 2014.
External links
Photo of an Ultimate 10-200
February 26, 2023
ultimate, canadian, homebuilt, aerobatic, biplane, that, designed, produced, streamline, welding, hamilton, ontario, introduced, 1990s, when, available, aircraft, supplied, form, plans, amateur, construction, role, homebuilt, aircraftnational, origin, canadama. The Ultimate 10 200 is a Canadian homebuilt aerobatic biplane that was designed produced by Streamline Welding of Hamilton Ontario introduced in the 1990s When it was available the aircraft was supplied as a kit or in the form of plans for amateur construction 1 Ultimate 10 200Role Homebuilt aircraftNational origin CanadaManufacturer Streamline WeldingIntroduction 1990sStatus Production completed Contents 1 Design and development 2 Operational history 3 Variants 4 Specifications Ultimate 10 200 5 See also 6 References 7 External linksDesign and development EditThe aircraft started out as a replacement set of wings for the Pitts Special and eventually a new fuselage was designed to go with the wing set The resulting aircraft features a strut braced biplane layout with cabane struts interplane struts and flying wires a single seat enclosed cockpit under a bubble canopy fixed conventional landing gear with wheel pants and a single engine in tractor configuration 1 The aircraft is made from metal with its flying surfaces covered in doped aircraft fabric Its wing span is only 16 00 ft 4 9 m The acceptable power range varies by each model Standard equipment includes an inverted fuel system and rear hinged canopy Operational g loads are 7 and 5 g The aircraft has a roll rate of 360 degrees per second 1 The 10 200 version has a typical empty weight of 925 lb 420 kg and a gross weight of 1 320 lb 600 kg giving a useful load of 395 lb 179 kg With full fuel of 22 U S gallons 83 L 18 imp gal the payload for the pilot and baggage is 263 lb 119 kg 1 The standard day sea level no wind take off with a 200 hp 149 kW engine is 450 ft 137 m and the landing roll is 500 ft 152 m 1 The manufacturer estimated the construction time from the supplied kit as 1200 hours 1 Operational history EditIn March 2014 six examples were registered in the United States with the Federal Aviation Administration although a total of 12 had been registered at one time Also in March 2014 two were registered in Canada with Transport Canada 2 3 Variants EditUltimate 10 180 Model powered by the 180 hp 134 kW Lycoming O 360 powerplant Ultimate 10 200 Model powered by the 200 hp 149 kW Lycoming IO 360 powerplant Ultimate 10 300 Model powered by the 300 hp 224 kW Lycoming IO 540 powerplantSpecifications Ultimate 10 200 EditData from AeroCrafter 1 General characteristicsCrew one Length 16 ft 6 in 5 03 m Wingspan 16 ft 0 in 4 88 m Empty weight 925 lb 420 kg Gross weight 1 350 lb 612 kg Fuel capacity 22 U S gallons 83 L 18 imp gal Powerplant 1 Lycoming IO 360 four cylinder air cooled four stroke aircraft engine 200 hp 150 kW Propellers 3 bladed constant speed propellerPerformance Maximum speed 220 mph 350 km h 190 kn Cruise speed 170 mph 270 km h 150 kn Stall speed 60 mph 97 km h 52 kn Range 500 mi 800 km 430 nmi Rate of climb 2 000 ft min 10 m s See also EditList of aerobatic aircraftReferences Edit a b c d e f g Purdy Don AeroCrafter Homebuilt Aircraft Sourcebook Fifth Edition page 264 BAI Communications 15 July 1998 ISBN 0 9636409 4 1 Federal Aviation Administration 15 March 2014 Make Model Inquiry Results Retrieved 15 March 2014 Transport Canada 15 March 2014 Canadian Civil Aircraft Register Archived from the original on 18 July 2011 Retrieved 15 March 2014 External links EditPhoto of an Ultimate 10 200 Retrieved from https en wikipedia org w index php title Ultimate 10 200 amp oldid 1089724608, wikipedia, wiki, book, books, library,
