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Ultraflight Lazair

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over developing a new propeller. Also, since inception, the Lazair was designed as a powered glider, so stacking of the two propellers in a bi-plane mode created a propeller that had less drag when gliding than if the 4 blades were 90 degrees apart. Any slight loss in thrust due to stacking was accepted since there was less drag when gliding.
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surfaces. All the wing panels had the same airfoil sections, planform, washout, wing tip design, aileron design and incidence to fuselage (including the two place). All the tail surfaces had the same airfoil (flat), planform (minor difference with different tailwheels), washout (none), distance from the wing and incidence to the fuselage.
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The propellers were the same plastic units used on the Series I with its 5.5 hp (4.1 kW) engines. To absorb the greater power two propellers were stacked to form a "biplane propeller". This was done because UltraFlight had ample supplies of the existing propellers and using them saved money
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Kramer opted for two engines instead of one because he wanted to use two of the largest chainsaw motors to obtain the total of 11 hp (8.2 kW) which he deemed necessary to make his "powered glider" fly with performance that was acceptable to him. He placed the two motors as close together as
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Performance was not as good as anticipated. Although Kramer did most of the test piloting, the lighter Peter Corley took it on its first flight in November 1978. The engines were subsequently moved from their original position below the wing to directly in front of the leading edge. The improvement
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During the production of the Series II the tail skids were replaced with tail wheels and later on, swiveling wheels. Skis were also available, although open cockpit flying in the winter could be a challenge. Rudder pedals were introduced which allowed side slipping of the aircraft as well as
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The first Lazair kits were originally marketed just under the model name "Lazair", but were later termed "Series I" after improved models had appeared. From the first Lazair prototype, to the last Lazair kit produced, no changes were made to the aerodynamic design of the wing panels and tail
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The initial model Lazair was a single-seater with a 36.3-foot (11.1 m) wingspan and was powered by two 5.5 hp 100 cc Pioneer chainsaw engines, directly driving plastic propellers in tractor configuration. The main landing gear used 16-inch (410 mm) wheels with a track of just
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International Fly-In and Expo, Florida, in March 1979. It won the award for best home-built microlight, repeating the accolade at Oshkosh that year and receiving thirty-three orders on the spot. Kramer began series production, with Corley as his first demonstration pilot.
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ultralight sailplane. Kramer took it to the next year's Oshkosh, where he met Ed Sweeney. Later they fitted it with two of Sweeney's engine kits. Kramer kept the engines and designed a new plane for them, which would remedy the deficiencies he saw in the Superfloater.
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The Lazair was thus built from standard aircraft materials, but it had many innovative design features for an ultralight, including the aerofoil, winglets, inverted-V tail and ruddervators, transparent film covered flying surfaces and twin engines.
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on the tail were interconnected so that turns were made with connected rudder and aileron by moving the stick to the side. Pitch control was via conventional fore-and-aft stick movement moving the ruddervators together as elevators.
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to be seen on a light aircraft. This combination produces an aircraft with optimized low-speed handling and very gentle stall characteristics. The high aspect ratio wing also made the Lazair a good glider, giving it a 12:1
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The Lazair Elite is a limited production aircraft that includes a structurally strengthened airframe using the Lazair II wings and an optional an enclosed cockpit. It is suitable for heavier pilots.
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There was customer demand for putting the Lazair on floats, but this required more power than the Pioneer powerplants could develop. The solution was to substitute 9.5 horsepower (7.1 kW)
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PET polymer film, attached to the airframe with single- and two-sided tapes. The Mylar proved to have a short service life due to UV damage, so it was eventually replaced by the more expensive
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A Lazair Series II displays the very long wing which gives this aircraft good gliding performance. This aircraft has been modified with conventional aircraft fabric and wider main landing gear.
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possible to reduce yaw when one failed. The Lazair was one of the first ultralights to incorporate twin engines, greatly improving the reliability and safety of this class of aircraft.
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As an ultralight aircraft designed for low flying speeds, the fuselage comprises an open frame of aluminum tube supporting the open cockpit, tricycle undercarriage and inverted-V tail.
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engines producing 26 hp (19 kW) each. The engines are more widely spaced than on the single-seater models which gives it different single engine handling characteristics.
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Later models incorporated many refinements and options including twin seating in tandem, more powerful engines, fuselage fairings and a conventional control stick pivot position.
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In the 21st century many Lazairs are still in use by private owners. As when first introduced, they remain prized for their handling qualities, if not their cruising speed.
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For control run simplicity the control stick pivot point was located above the pilot with the stick hanging downwards. Conventional ailerons together with tail
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In November 2007 the Canadian register still carried a total of 460 Lazairs of all models. In the USA where the majority of Lazairs are flown as unregistered
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The Lazair II is a two-seater trainer with the seats in side-by-side configuration. It was introduced in 1983 and approximately 50 Lazair II kits were sold.
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A Lazair II two-seat trainer has one of its JPX PUL 425 engines started. Lazairs generally do not have electrical systems, and their engines are started by
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JM1 powerplants with Jeti SPIN Pro 300 controllers and dual 16 cell 4 amp-hour battery packs that produce 63 volts, mounted in the wings. The aircraft won
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A Lazair Series III with its bottom-mounted control stick. This one has been modified with a streamlined pod and windshield. The engines are the
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The wing is mounted at the top of the fuselage frame with additional outboard diagonal bracing struts. It is of straight, constant taper, high
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engines. These single-cylinder engines were used extensively in forest fire fighting water pumps and had proved reliable in that application.
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crosswind landings. The rudders could be coupled to the ailerons or de-coupled and controlled by the pedals in flight through a mixer gear.
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It was one of the first twin-engined ultralights. More Lazairs have been registered in Canada than any other type of Canadian aircraft.
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Production ended in 1984, the company citing "liability concerns" and the resulting cost and availability of insurance as the reason.
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26 inches, which combined with the long wing span, meant that taxiing in more than 7 mph (11 km/h) of wind required a
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He started with a blank sheet of paper and designed a completely new aircraft, the Lazair, even going so far as to design a custom
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planform. The airfoil section is of Kramer's own design and incorporates reverse camber at the trailing edge, giving an S-shaped
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provided full three-axis control, which although standard on conventional aircraft was unusual for ultralights at the time. The
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convention in 1977, where he saw the potential of the ultralight aircraft present. He built and flew an early type of
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The "SS" is the "Surveillance Special" which was designed for police use, which included the Elite airframe and the
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of Canadian design, as a contraction of "lazy air" due to the slow cruising speed, and as an allusion to "
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The first Lazair prototype was constructed by Kramer with some help from Corley and first flown in 1978.
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The Lazair inspired many other aircraft designers to use the Lazair wing construction techniques. The
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in performance proved definitive and in this form they demonstrated the prototype Lazair at the EAA
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The third series of the single-seat Lazair introduced customer-requested upgrades, such as:
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The Lazair I is a single-seat conventional high-wing monoplane with an open fuselage frame,
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In 1979, Kramer formed UltraFlight Incorporated to produce the design in his home town of
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for it. He named it Lazair for several reasons, including a reference to the successful
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It may require cleanup to comply with Knowledge (XXG)'s content policies, particularly
1919: 1643: 1638: 1312:, Kitplanes, Volume 28, Number 12, December 2011, pages 31-35. Belvoir Publications. 909: 829: 607:
at AirVenture. The aircraft is an experimental project and no production is planned.
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Dale Kramer; "Remembering Peter Corley: and the birth of the Lasair ultralight",
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Power on the Series III is still provided by two 9.5 horsepower (7.1 kW)
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Choosing Your Homebuilt - the one you will finish and fly! Second Edition
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KFM 25 hp (19 kW) engines also used on the two-seat Lazair II.
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engines with the option of a pair of KFM 25 hp (19 kW) or
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Official Gazette of the United States Patent and Trademark office
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The only Lazair SS EC aircraft ever produced was employed by the
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9.5 hp two-stroke powerplants driving "biplane" propellers.
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In 2011 Lazair designer Dale Kramer introduced an experimental
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Lazair on an amphibious mono-float, with outrigger floats at
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is one aircraft that uses a wing based on the Lazair wing.
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8th Edition, page E-21. Cybair Limited Publishing, 2001.
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A major contributor to this article appears to have a
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Aircraft of comparable role, configuration, and era
1048:, pages 98-106. Kitplanes Magazine, December 2000. 976:, pages 64-70. Kitplanes Magazine, September 2000. 236:that were sold in kit form between 1979 and 1984. 501:landing gear widened to 46 inches (1,200 mm) 469:. Tail skids were fitted to the inverted V-tail. 1150:, pages 76-83. Kitplanes Magazine, October 2000. 932:, Volume 1042 Number 2, Trademarks May 8, 1984. 629:In the USA the single-seat models are flown as 1220: 1218: 1216: 1214: 1026:, Issue 2004/4 August/September, 2004, Page 4. 713:Custom Lazair airfoil, reflexed top and bottom 443:ultralights there were also ten registered as 1439: 8: 332:. It also features some of the first modern 1368:"Ultra-light Aeroplane Transition Strategy" 1058: 1056: 1054: 1446: 1432: 1424: 1018: 1016: 1014: 316:. The wing has a progressive and constant 1349:, page 195-201. Butterfield Press, 1993. 1284:"FAA Registry Make/Model Inquiry Results" 1117: 1115: 184:A Lazair Series III showing the original 64:Learn how and when to remove this message 1454:Uncertified aircraft developed in Canada 1094: 1092: 1090: 1088: 1086: 1084: 1082: 1080: 1078: 1076: 968: 966: 964: 962: 960: 958: 795:3.14 lb/sq ft (15.4 kg/m) 622:In Canada all Lazairs are classified as 510:conventional floor-mounted control stick 246:issued a stamp in honour of the Lazair. 1164: 1162: 1160: 1158: 1156: 1142: 1140: 1040: 1038: 1036: 1034: 956: 954: 952: 950: 948: 946: 944: 942: 940: 938: 922: 777:135 mi (217 km, 117 nmi) 756:40 mph (65 km/h, 35 kn) 1336:, COPA Flight, page C-1, February 2005 1334:Canadian Owners and Pilots Association 1277: 1275: 1169:National Air and Space Museum (1998). 771:60 mph (97 km/h, 52 kn) 762:17 mph (28 km/h, 15 kn) 750:55 mph (89 km/h, 48 kn) 204:A Lazair II two-seat trainer with its 77: 7: 1252:Transport Canada (1 November 2007). 360:, foam ribs and an aluminum tubular 1310:Dale Kramer and his electric Lazair 1146:Hunt, Adam & Ruth Merkis-Hunt: 1124:"Lazair: A Classic Ultralight Twin" 1100:Ultralight Aircraft Shopper's Guide 1044:Hunt, Adam & Ruth Merkis-Hunt: 991:"Details magazine No. 3 March 2019" 972:Hunt, Adam & Ruth Merkis-Hunt: 208:engines of 26 hp (19 kW). 1926:1970s Canadian ultralight aircraft 1366:Transport Canada (17 April 2007). 1254:"Canadian Civil Aircraft Register" 692:36 ft 4 in (11.1 m) 686:13 ft 0 in (3.96 m) 595:. The aircraft is powered by twin 507:for increased negative-g tolerance 14: 704:143 sq ft (13.3 m) 698:6 ft 4 in (1.92 m) 659:Specifications (Lazair Series II) 525:26 hp (19 kW) engines. 420:The aircraft were widely sold in 1171:"Ultraflight Sales Lazair SS EC" 820:American Aerolights Double Eagle 544:The Lazair II is powered by two 352:The wing structure comprises an 86: 44:. Please discuss further on the 23: 1396:List of Lazairs by registration 1227:"An introduction to the Lazair" 232:designed and built twin-engine 188:covered wings and tail surfaces 107:and police observation aircraft 1070:, August 1, 1982, pages 10-16. 789:200 ft/min (1.0 m/s) 1: 1946:Twin-engined tractor aircraft 1415:"Light Stuff" (Lazair review) 783:11,000 ft (3,350 m) 302:and twin tractor propellers. 95:UltraFlight Lazair Series II 1941:Aircraft first flown in 1978 16:Canadian ultralight aircraft 1068:The Financial Post Magazine 680:240 lb (109 kg) useful load 652:Steven F. Udvar-Hazy Center 639:experimental amateur-builts 601:Antique Ultralight Champion 1967: 900:US Aviation Super Floater 725:450 lb (204 kg) 583:Electric Lazair (eLazair) 94: 85: 80: 1823:Freedom Lite/Legend Lite 1046:Test Flying Lazair No. 1 850:Blue Yonder EZ Fun Flyer 804:23.7 lb/hp (0.069 kW/kg) 719:210 lb (95 kg) 451:Variants and derivatives 254:Dale Kramer visited the 905:Wolford-Wilson Sailwing 875:Jean St-Germain Raz-Mut 825:AmEagle American Eaglet 735:, 9.5 hp (7.1 kW) each 665:General characteristics 1783:Nordic 8 Mini Explorer 890:Mitchell U-2 Superwing 885:Milholland Legal Eagle 579: 412:Port Colborne, Ontario 221: 209: 197: 189: 177: 1811:Aerocruiser 450 Turbo 1417:, December 16, 2007, 1407:postagestampguide.com 1401:Postage Stamp Guide. 1225:Lazair Force (n.d.). 1064:"Success on the Wing" 577: 567:Police Department in 215: 203: 195: 183: 171: 103:Ultralight personal, 42:neutral point of view 1578:Bushcaddy/CADI/CLASS 1568:Twin Engine EZ Flyer 1345:Armstrong, Kenneth: 895:Pterodactyl Ascender 650:Lazair SS EC at the 605:Ultralight Amphibian 275:Laser sailing dinghy 1196:Lazair.com (n.d.). 723:Max takeoff weight: 645:Aircraft on display 432:Operational history 234:ultralight aircraft 1951:High-wing aircraft 1931:Homebuilt aircraft 1821:Spectrum Aircraft/ 1469:Beaver RX 550 Plus 1233:on 14 October 2006 1177:on 10 October 2007 870:Gemini Hummingbird 865:Eipper Quicksilver 767:Never exceed speed 624:Basic Ultra-lights 612:Blue Yonder Merlin 580: 447:in November 2007. 341:, and it could be 322:angle of incidence 320:, or reduction in 226:UltraFlight Lazair 222: 210: 198: 190: 178: 1913: 1912: 1697:Froebe helicopter 1122:UL Flyer (n.d.). 860:Chotia Weedhopper 618:Regulatory status 166: 165: 130:UltraFlight Inc. 74: 73: 66: 37:with its subject. 1958: 1806:Aerocruiser Plus 1448: 1441: 1434: 1425: 1410: 1384: 1383: 1381: 1379: 1374:on 10 April 2009 1370:. 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112: 111: 108: 101: 97: 96: 92: 91: 83: 82: 81:Lazair series 72: 71: 31: 29: 22: 15: 13: 10: 9: 6: 4: 3: 2: 1963: 1952: 1949: 1947: 1944: 1942: 1939: 1937: 1934: 1932: 1929: 1927: 1924: 1923: 1921: 1906: 1903: 1901: 1898: 1896: 1893: 1891: 1888: 1887: 1885: 1883: 1879: 1873: 1870: 1869: 1867: 1865: 1861: 1855: 1852: 1851: 1849: 1847: 1843: 1837: 1834: 1832: 1829: 1828: 1826: 1824: 1818: 1812: 1809: 1807: 1804: 1802: 1799: 1798: 1796: 1794: 1790: 1784: 1781: 1779: 1776: 1774: 1771: 1769: 1766: 1764: 1761: 1759: 1756: 1754: 1751: 1749: 1746: 1744: 1741: 1740: 1738: 1736: 1732: 1726: 1723: 1721: 1718: 1716: 1713: 1712: 1710: 1708: 1704: 1698: 1695: 1694: 1692: 1690: 1686: 1680: 1677: 1675: 1672: 1670: 1667: 1665: 1662: 1660: 1657: 1655: 1652: 1650: 1647: 1645: 1642: 1640: 1637: 1635: 1632: 1630: 1627: 1625: 1622: 1620: 1617: 1615: 1612: 1611: 1609: 1607: 1603: 1597: 1594: 1592: 1589: 1587: 1584: 1583: 1581: 1579: 1575: 1569: 1566: 1564: 1563:EZ King Cobra 1561: 1559: 1556: 1554: 1551: 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Index

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neutral point of view
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trainer aircraft
Canada

Rotax 185

Tedlar


JPX PUL 425

recoil start
Canadian
ultralight aircraft
Canada Post
Oshkosh
EAA
Superfloater
airfoil
Laser sailing dinghy
laissez-faire
Sun 'n Fun
inverted V-tail
aspect ratio
camber line
washout

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