Ultralight Aircraft
-
Upload
jerry-goffman -
Category
Technology
-
view
11.849 -
download
36
description
Transcript of Ultralight Aircraft
![Page 1: Ultralight Aircraft](https://reader035.fdocuments.net/reader035/viewer/2022081415/558366f1d8b42a9c2b8b4b65/html5/thumbnails/1.jpg)
Ultralight Aircraft of Ultralight Aircraft of the the
U.S.A.U.S.A.
![Page 2: Ultralight Aircraft](https://reader035.fdocuments.net/reader035/viewer/2022081415/558366f1d8b42a9c2b8b4b65/html5/thumbnails/2.jpg)
A presentation of Virtualultralightmuseum.com
Jerry M. Goffman, Curator
![Page 3: Ultralight Aircraft](https://reader035.fdocuments.net/reader035/viewer/2022081415/558366f1d8b42a9c2b8b4b65/html5/thumbnails/3.jpg)
These unique aircraft can be flown with no pilot's license, no insurance and no Medical Certificate.
![Page 4: Ultralight Aircraft](https://reader035.fdocuments.net/reader035/viewer/2022081415/558366f1d8b42a9c2b8b4b65/html5/thumbnails/4.jpg)
Building these aircraft takes a minimum amount of time and few tools. Average building time can be less than 200 hours.
![Page 5: Ultralight Aircraft](https://reader035.fdocuments.net/reader035/viewer/2022081415/558366f1d8b42a9c2b8b4b65/html5/thumbnails/5.jpg)
There are limitations where these aircraft can be flown, but you can soar like an eagle for a hour's time and Realize an American Dream.
![Page 6: Ultralight Aircraft](https://reader035.fdocuments.net/reader035/viewer/2022081415/558366f1d8b42a9c2b8b4b65/html5/thumbnails/6.jpg)
A-10A-10
Designed by Don Mitchell. Powered glider from late 70's. Aluminum wing covering. Empty weight 280 lbs. Structural limits +4 Gs and -2.3 Gs.
![Page 7: Ultralight Aircraft](https://reader035.fdocuments.net/reader035/viewer/2022081415/558366f1d8b42a9c2b8b4b65/html5/thumbnails/7.jpg)
Aerolite 103Aerolite 103
Assembled and ready to fly. Empty weight 250 lbs. Useful load 270 lbs. Cruise speed 55 mph and stall speed 28 mph. Structural limits are +4 Gs and -2.8 Gs.
![Page 8: Ultralight Aircraft](https://reader035.fdocuments.net/reader035/viewer/2022081415/558366f1d8b42a9c2b8b4b65/html5/thumbnails/8.jpg)
Aeroplane XPAeroplane XP
A 3-axis, open cockpit biplane. Empty weight 225 lbs. Payload 250 lbs. Stall speed 19 mph. 100 fpm climb rate. Load factors +6 Gs and -4 Gs.
![Page 9: Ultralight Aircraft](https://reader035.fdocuments.net/reader035/viewer/2022081415/558366f1d8b42a9c2b8b4b65/html5/thumbnails/9.jpg)
Aerosport Raile MkII (1970)Aerosport Raile MkII (1970)
H.L. Wood is the designer. Easy build low wing monoplane. Rockwell JLO LB-600 snow mobile power plants weighing about 56 lbs and developing 33 hp.
![Page 10: Ultralight Aircraft](https://reader035.fdocuments.net/reader035/viewer/2022081415/558366f1d8b42a9c2b8b4b65/html5/thumbnails/10.jpg)
Aerotique ParasolAerotique Parasol
Constructed from gusset reinforced rectangular tubing. The fuselage weighs 12 lbs. Empty weight 250 lbs. Payload 270 lbs. Cruise speed 60 mph and stall speed 24 mph.
![Page 11: Ultralight Aircraft](https://reader035.fdocuments.net/reader035/viewer/2022081415/558366f1d8b42a9c2b8b4b65/html5/thumbnails/11.jpg)
Airbike (1994)Airbike (1994)
A conventional hi-wing monoplane and the pilot rides it like a bicycle. This is a 3-Axis aircraft with removable wings. Structural limits +4 Gs and -2 Gs.
![Page 12: Ultralight Aircraft](https://reader035.fdocuments.net/reader035/viewer/2022081415/558366f1d8b42a9c2b8b4b65/html5/thumbnails/12.jpg)
Airey-PlaneAirey-Plane
Wilbur Staib built this small airplane in limited hangar space. Two 10 hp West Bend 820 chain-saw engines. Net weight 175 lbs.
![Page 13: Ultralight Aircraft](https://reader035.fdocuments.net/reader035/viewer/2022081415/558366f1d8b42a9c2b8b4b65/html5/thumbnails/13.jpg)
Ascender IIIB (1975)Ascender IIIB (1975)
Designed by Jack McCornack. Essentially a weight shift controlled, wire braced flying wing. Empty weight 215 lbs. Payload 300 lbs. Build time estimated at 100 hrs.
![Page 14: Ultralight Aircraft](https://reader035.fdocuments.net/reader035/viewer/2022081415/558366f1d8b42a9c2b8b4b65/html5/thumbnails/14.jpg)
Astra (1983)Astra (1983)
Designed by Ian Becker and Walt Todhunter. Single-seat, high-wing monoplane with 3-Axis control. Empty weight 248 lbs. Structural limits +6 Gs and -4 Gs.
![Page 15: Ultralight Aircraft](https://reader035.fdocuments.net/reader035/viewer/2022081415/558366f1d8b42a9c2b8b4b65/html5/thumbnails/15.jpg)
AvengerAvenger
High-wing, 3-axis monoplane with cable braced wing. 30 hp Kawasaki 440 engine. Empty weight 252 lbs.
![Page 16: Ultralight Aircraft](https://reader035.fdocuments.net/reader035/viewer/2022081415/558366f1d8b42a9c2b8b4b65/html5/thumbnails/16.jpg)
Avion (1982)Avion (1982) Designed by Bob Lovejoy.
Cruise speed 48 mph, stall speed 27 mph. Load factors +6 Gs and-4 Gs. Empty weight 250 lbs. Payload 280 lbs.
![Page 17: Ultralight Aircraft](https://reader035.fdocuments.net/reader035/viewer/2022081415/558366f1d8b42a9c2b8b4b65/html5/thumbnails/17.jpg)
B1RDB1RD
First major aircraft company to manufacture an ultralight airplane. Empty weight 220 lbs. Load factors +3 Gs and -2 Gs.
![Page 18: Ultralight Aircraft](https://reader035.fdocuments.net/reader035/viewer/2022081415/558366f1d8b42a9c2b8b4b65/html5/thumbnails/18.jpg)
Backyard FlyerBackyard Flyer
All welded aluminum construction. Wing swings parallel to fuselage for easy transport. Empty weight 254 lbs. Rate of climb 800 fpm.
![Page 19: Ultralight Aircraft](https://reader035.fdocuments.net/reader035/viewer/2022081415/558366f1d8b42a9c2b8b4b65/html5/thumbnails/19.jpg)
Banchee (1982)Banchee (1982)
Designed by Brian Jensen, Gill Kinzie and Nick Nichols. Hi-wing monoplane with canard. Cruise speed 35 mph. Stalls at 22 mph. Empty weight 251 lbs. Structural limits +6 Gs and -4Gs.
![Page 20: Ultralight Aircraft](https://reader035.fdocuments.net/reader035/viewer/2022081415/558366f1d8b42a9c2b8b4b65/html5/thumbnails/20.jpg)
Banty (1985)Banty (1985)
High wing parasol type aircraft with wood and fabric construction. Estimated 500 hr. build time. Empty weight 237 lbs. Cruise speed 50 mph and stalls at 27 mph. Climb rate 400 fpm.
![Page 21: Ultralight Aircraft](https://reader035.fdocuments.net/reader035/viewer/2022081415/558366f1d8b42a9c2b8b4b65/html5/thumbnails/21.jpg)
Beachy Breezer (1984)Beachy Breezer (1984)
Designed by Clair O’Meyer. Empty weight 245 lbs. Payload 265 lbs. Load factors +4 Gs and -3 Gs. Cruise speed 48 mph and stall speed 20 mph.
![Page 22: Ultralight Aircraft](https://reader035.fdocuments.net/reader035/viewer/2022081415/558366f1d8b42a9c2b8b4b65/html5/thumbnails/22.jpg)
Beaujon Mach .07Beaujon Mach .07
Plans built. Empty weight 160 lbs. Useful load 225 lbs. Building time 60-80 hrs. Cruise speed 38 mph and stall speed 20 mph. Climb rate 350 fpm.
![Page 23: Ultralight Aircraft](https://reader035.fdocuments.net/reader035/viewer/2022081415/558366f1d8b42a9c2b8b4b65/html5/thumbnails/23.jpg)
Birdman TL-1B (1975)Birdman TL-1B (1975)
Designed by Emmett M. Talley. Aluminum and wood with 2-Axis controls. Empty weight 130 lbs. Glide ratio 15:1
![Page 24: Ultralight Aircraft](https://reader035.fdocuments.net/reader035/viewer/2022081415/558366f1d8b42a9c2b8b4b65/html5/thumbnails/24.jpg)
Babybird DS-1 (1984)Babybird DS-1 (1984)
Designed by Donald Stits as World's Smallest Plane. Empty weight 250 lbs. Payload 188 lbs. Cruise speed 88 mph and climb rate of 925 fpm.
![Page 25: Ultralight Aircraft](https://reader035.fdocuments.net/reader035/viewer/2022081415/558366f1d8b42a9c2b8b4b65/html5/thumbnails/25.jpg)
Boxmouth (1975)Boxmouth (1975)
Easy to build requiring local supplies from hardware and farming equipment supply stores. Wings at front and rear.
![Page 26: Ultralight Aircraft](https://reader035.fdocuments.net/reader035/viewer/2022081415/558366f1d8b42a9c2b8b4b65/html5/thumbnails/26.jpg)
Buzzard MG-1Buzzard MG-1
Designed by Bud Snyder. Essentially a motorized glider with a parasol wing. Empty weight 200 lbs, Payload 275 lbs. Glide ratio 15:1.
![Page 27: Ultralight Aircraft](https://reader035.fdocuments.net/reader035/viewer/2022081415/558366f1d8b42a9c2b8b4b65/html5/thumbnails/27.jpg)
CadetCadet
Tractor engine, aluminum tube monoplane with sailcloth wing. Empty weight 248 lbs. Payload 303 lbs. Structural limits +6 Gs and -4 Gs.
![Page 28: Ultralight Aircraft](https://reader035.fdocuments.net/reader035/viewer/2022081415/558366f1d8b42a9c2b8b4b65/html5/thumbnails/28.jpg)
Calypso (1984)Calypso (1984)
Double surface wings. Cruise speed 50 mph, stall speed 27 mph. Climb rate 800 fpm. Empty weight 278 lbs. Payload 222 lbs. Load factors +6 Gs and -4 Gs.
![Page 29: Ultralight Aircraft](https://reader035.fdocuments.net/reader035/viewer/2022081415/558366f1d8b42a9c2b8b4b65/html5/thumbnails/29.jpg)
Challenger IChallenger I
Factory built airframe and wings. Estimated 100 hours assembly time. Empty weight 235 lbs. Payload 258 lbs. Load factors +4 Gs and -3 Gs.
![Page 30: Ultralight Aircraft](https://reader035.fdocuments.net/reader035/viewer/2022081415/558366f1d8b42a9c2b8b4b65/html5/thumbnails/30.jpg)
Chandelle Mk IVChandelle Mk IV
Designed by Nile Downer. Aluminum alloy tube airframe. Empty weight 243 lbs. Payload 257 lbs. Cruise speed 40 mph and stall speed 22 mph. Climb rate 650 fpm.
![Page 31: Ultralight Aircraft](https://reader035.fdocuments.net/reader035/viewer/2022081415/558366f1d8b42a9c2b8b4b65/html5/thumbnails/31.jpg)
Citizen FlyCitizen Fly
Composite materials. Building time approx. 56 hrs. Empty weight 254 lbs. Cruise speed 55 mph, landing speed 27 mph. Climb rate 700 fpm. Structural limits +6 Gs and -4 Gs.
![Page 32: Ultralight Aircraft](https://reader035.fdocuments.net/reader035/viewer/2022081415/558366f1d8b42a9c2b8b4b65/html5/thumbnails/32.jpg)
Clipper (1984)Clipper (1984)
Designed by Fred Bell. Empty weight 252 lbs. Payload 346 lbs. Cruise speed 60 mph and stalls at 25 mph. Climb rate 800 fpm. Structural limits +6 Gs and -4 Gs.
![Page 33: Ultralight Aircraft](https://reader035.fdocuments.net/reader035/viewer/2022081415/558366f1d8b42a9c2b8b4b65/html5/thumbnails/33.jpg)
Cloudbuster (1981)Cloudbuster (1981)
Powered glider with tractor engine. Aluminum, and composite construction. Empty weight 248 lbs. Structural limits +4.5 Gs and -2.25 Gs. Glide ratio 13:1.
![Page 34: Ultralight Aircraft](https://reader035.fdocuments.net/reader035/viewer/2022081415/558366f1d8b42a9c2b8b4b65/html5/thumbnails/34.jpg)
Cloud Dancer (1983)Cloud Dancer (1983)
V-tail powered glider designed by Erwin Rodger and Delura Roger. Aluminum tube, and dacron sail cloth. Empty weight 252 lbs. Payload 252 lbs. Structural limits +4.2 Gs and -2 Gs.
![Page 35: Ultralight Aircraft](https://reader035.fdocuments.net/reader035/viewer/2022081415/558366f1d8b42a9c2b8b4b65/html5/thumbnails/35.jpg)
Cloud RiderCloud Rider
Low front mounted engine with tricycle landing gear and strut braced double surface wing. 3-axis control.
![Page 36: Ultralight Aircraft](https://reader035.fdocuments.net/reader035/viewer/2022081415/558366f1d8b42a9c2b8b4b65/html5/thumbnails/36.jpg)
Cloudster (1999)Cloudster (1999)
Wood with metal struts. Pilots legs extended outside the fuselage to the rudder pedals. Empty weight 250 lbs. Cruise 50 mph, stall 22 mph, and climb rate 700 fpm.
![Page 37: Ultralight Aircraft](https://reader035.fdocuments.net/reader035/viewer/2022081415/558366f1d8b42a9c2b8b4b65/html5/thumbnails/37.jpg)
Cobra (1982)Cobra (1982)
Designed by Wayne and Kerry Richter. Cruise speed 50 mph, stall speed 24 mph. and climb rate at 1000 fpm. Empty weight 235 lbs. Payload 280 lbs. Load factors +5 Gs and -3 Gs.
![Page 38: Ultralight Aircraft](https://reader035.fdocuments.net/reader035/viewer/2022081415/558366f1d8b42a9c2b8b4b65/html5/thumbnails/38.jpg)
CondorCondor
Designed by Buddy Head, Bob Carswell and Dave French. Climb rate 775 fpm Empty weight 245 lbs. Structural limits: +5 Gs and -3 Gs. Build time 75 hrs.
![Page 39: Ultralight Aircraft](https://reader035.fdocuments.net/reader035/viewer/2022081415/558366f1d8b42a9c2b8b4b65/html5/thumbnails/39.jpg)
Cumulus (1996)Cumulus (1996)
Useful load 280 lbs. Cruise speed 60 mph and stall speed 32 mph. Load factors +4 Gs and -2 Gs. Glide ratio 20:1. Approximate build time is 150 hrs.
![Page 40: Ultralight Aircraft](https://reader035.fdocuments.net/reader035/viewer/2022081415/558366f1d8b42a9c2b8b4b65/html5/thumbnails/40.jpg)
Diehl XTC (1982)Diehl XTC (1982)
An amphibian in a pusher configuration. Canard with twin tail rudders. Retractable wheels. Empty Weight 240 lbs. Payload 230 lbs. Build time approximately 400 hrs.
![Page 41: Ultralight Aircraft](https://reader035.fdocuments.net/reader035/viewer/2022081415/558366f1d8b42a9c2b8b4b65/html5/thumbnails/41.jpg)
Dream ClassicDream Classic
Akin to the 1907 Demoiselle. Estimated construction kit build time 100-200 hrs. Empty weight 241 lbs. Cruises at 57 mph, stalls at 26 mph and climbs at 850 fpm.
![Page 42: Ultralight Aircraft](https://reader035.fdocuments.net/reader035/viewer/2022081415/558366f1d8b42a9c2b8b4b65/html5/thumbnails/42.jpg)
Eagle (1975)Eagle (1975)
Designed by Larry Hair. Single-seat, high-wing, monoplane with canard wing. Build time is 75 hrs. Empty weight 170 lbs. Structural limits +8 Gs and -2.5 Gs.
![Page 43: Ultralight Aircraft](https://reader035.fdocuments.net/reader035/viewer/2022081415/558366f1d8b42a9c2b8b4b65/html5/thumbnails/43.jpg)
Easy Riser (1975)Easy Riser (1975)
Originally flown by John Moody. Pusher bi-plane. Aluminum tube and sailcloth. Wire braced wing. Hybrid control system. Empty weight 120 lbs.
![Page 44: Ultralight Aircraft](https://reader035.fdocuments.net/reader035/viewer/2022081415/558366f1d8b42a9c2b8b4b65/html5/thumbnails/44.jpg)
Eclipse (1983)Eclipse (1983)
Designed by J. Bruce Emmons. Elliptical wing and inverted V-tail. Empty weight 165 lbs. Structural limits +9 Gs and -9 Gs. Glide ratio 15:1.
![Page 45: Ultralight Aircraft](https://reader035.fdocuments.net/reader035/viewer/2022081415/558366f1d8b42a9c2b8b4b65/html5/thumbnails/45.jpg)
EZ-1 (1983)EZ-1 (1983)
Designed by Richard Jiminez. Empty weight 234 lbs. Payload 271 lbs. Load factors +9 Gs and -4.5 Gs. Glide ratio 8:1
![Page 46: Ultralight Aircraft](https://reader035.fdocuments.net/reader035/viewer/2022081415/558366f1d8b42a9c2b8b4b65/html5/thumbnails/46.jpg)
Falcon (1982)Falcon (1982)
Designed by Romuald Drlik as a flying wing with canard. Empty weight 250 lbs. Payload 255 lbs. Load factors +5.8 Gs and -2.9 Gs.
![Page 47: Ultralight Aircraft](https://reader035.fdocuments.net/reader035/viewer/2022081415/558366f1d8b42a9c2b8b4b65/html5/thumbnails/47.jpg)
Firebird Flyer (1983)Firebird Flyer (1983)
Designed by Robert J. Davis and John T. Venaleck. 3-Axis single-seat, high-wing monoplane with inverted V-tail and pusher engine.
![Page 48: Ultralight Aircraft](https://reader035.fdocuments.net/reader035/viewer/2022081415/558366f1d8b42a9c2b8b4b65/html5/thumbnails/48.jpg)
Firestar IFirestar I
Designed by Homer Kolb. Empty weight 250 lbs. Payload 295 lbs. Structural limits +4 Gs and -2 Gs. Cruise speed 53 mph and climb rate 650 fpm.
![Page 49: Ultralight Aircraft](https://reader035.fdocuments.net/reader035/viewer/2022081415/558366f1d8b42a9c2b8b4b65/html5/thumbnails/49.jpg)
Flitplane (1995)Flitplane (1995)
Designed by Ed Fisher. Triangular windshield. Fuselage comes already welded. Estimated 150 hrs. build time from kit and 600 hrs. from plans. Empty weight 225 lbs.
![Page 50: Ultralight Aircraft](https://reader035.fdocuments.net/reader035/viewer/2022081415/558366f1d8b42a9c2b8b4b65/html5/thumbnails/50.jpg)
FlyerFlyer
Homer Kolb designer. Single seat, twin tractor engines. Empty weight 185 lbs. Structural limits +4Gs and -2.5 Gs.
![Page 51: Ultralight Aircraft](https://reader035.fdocuments.net/reader035/viewer/2022081415/558366f1d8b42a9c2b8b4b65/html5/thumbnails/51.jpg)
FP-303 (1984)FP-303 (1984)
Lexan canopy. Construction kit requires 400 hrs. build time. Empty weight 235 lbs. Payload 215 lbs. Structural limits +4.6 Gs and -2.3 Gs.
![Page 52: Ultralight Aircraft](https://reader035.fdocuments.net/reader035/viewer/2022081415/558366f1d8b42a9c2b8b4b65/html5/thumbnails/52.jpg)
Goldwing (1979)Goldwing (1979)
Designed by Craig Catto and Brian Glenn. Pusher engine with canard wing. Empty weight 220 lbs. Payload 260 lbs. Load factors +6 Gs and -4.5 Gs. Glide ratio 16:1.
![Page 53: Ultralight Aircraft](https://reader035.fdocuments.net/reader035/viewer/2022081415/558366f1d8b42a9c2b8b4b65/html5/thumbnails/53.jpg)
Gypsy(1980)Gypsy(1980)
Designed by John Chotia. Airframe of aluminum tubes bolted together. 3-Axis control. Empty weight 165 lbs.
![Page 54: Ultralight Aircraft](https://reader035.fdocuments.net/reader035/viewer/2022081415/558366f1d8b42a9c2b8b4b65/html5/thumbnails/54.jpg)
Home DepotHome Depot
Designed by Jack Harper from materials purchased from the Home Depot. The plane utilizes all wood construction. Uses two 10 HP Tecumseh motors.
![Page 55: Ultralight Aircraft](https://reader035.fdocuments.net/reader035/viewer/2022081415/558366f1d8b42a9c2b8b4b65/html5/thumbnails/55.jpg)
Huber Aero 101-1 (1983)Huber Aero 101-1 (1983)
Designed by James Huber. Fiberglass cockpit. Cruising speed 65 mph, stall speed 27 mph. Empty weight 220 lbs. Structural limits +5.2 Gs and – 2.8 Gs.
![Page 56: Ultralight Aircraft](https://reader035.fdocuments.net/reader035/viewer/2022081415/558366f1d8b42a9c2b8b4b65/html5/thumbnails/56.jpg)
Hummel CA-2Hummel CA-2
All aluminum aircraft that requires 600 hrs. build time. Structural loads are +4.4 Gs and -2.2 Gs. Empty weight 250 lbs.
![Page 57: Ultralight Aircraft](https://reader035.fdocuments.net/reader035/viewer/2022081415/558366f1d8b42a9c2b8b4b65/html5/thumbnails/57.jpg)
Hummer (1977)Hummer (1977)
Klaus Hill designed monoplane with pusher engine and V-tail. 2-Axis control. Empty weight 185 lbs. Payload 255 lbs. Structural limits +4 Gs and -3 Gs.
![Page 58: Ultralight Aircraft](https://reader035.fdocuments.net/reader035/viewer/2022081415/558366f1d8b42a9c2b8b4b65/html5/thumbnails/58.jpg)
Hummingbird SportHummingbird Sport
Designed by Ed Sweeney. Engines were Partner 8hp chain saws. Takeoff and landing speed was 15 mph and top speed was 55 mph. Empty weight 150 lbs.
![Page 59: Ultralight Aircraft](https://reader035.fdocuments.net/reader035/viewer/2022081415/558366f1d8b42a9c2b8b4b65/html5/thumbnails/59.jpg)
Hurricane 103 (1991)Hurricane 103 (1991)
Designed by Donnie Eccker. Empty weight 249 lbs. Payload 243 lbs. Cruise speed 65 mph, stalls at 27 mph. Buildtime 100 hrs.
![Page 60: Ultralight Aircraft](https://reader035.fdocuments.net/reader035/viewer/2022081415/558366f1d8b42a9c2b8b4b65/html5/thumbnails/60.jpg)
Huski/Coyote (1978)Huski/Coyote (1978)
Aluminum tubing and sailcloth. Hybrid control system. Cruise speed 43 mph and stalls at 22 mph. Climb rate 800 ft/min. Empty weight 198 lbs.
![Page 61: Ultralight Aircraft](https://reader035.fdocuments.net/reader035/viewer/2022081415/558366f1d8b42a9c2b8b4b65/html5/thumbnails/61.jpg)
Indiana FlyerIndiana Flyer
Designed by Lee Brazy. Shoulder wing monoplane. Cruise speed 42 mph and stalls at 30 mph. Empty weight 233 lbs. Payload 225 lbs.
![Page 62: Ultralight Aircraft](https://reader035.fdocuments.net/reader035/viewer/2022081415/558366f1d8b42a9c2b8b4b65/html5/thumbnails/62.jpg)
Invader MkIII (1982)Invader MkIII (1982)
Designed by Nick Leighty and Rick Berstling. Single seat, mid-wing with V-tail. Empty weight 245 lbs. Payload 230 lbs. Structural limits +4 Gs and -4 Gs. Glide ratio 14:1.
![Page 63: Ultralight Aircraft](https://reader035.fdocuments.net/reader035/viewer/2022081415/558366f1d8b42a9c2b8b4b65/html5/thumbnails/63.jpg)
Javelin I (1996)Javelin I (1996)
Cruise speed 60 mph, stall speed 26 mph. Climb rate 700 fpm. Estimated build time 80 hrs. Structural limits +4 Gs and -2 Gs. Empty weight 240 lbs.
![Page 64: Ultralight Aircraft](https://reader035.fdocuments.net/reader035/viewer/2022081415/558366f1d8b42a9c2b8b4b65/html5/thumbnails/64.jpg)
Kasperwing I-80 (1976)Kasperwing I-80 (1976)
Designed by W. Kasper in collaboration with Steve Grossruck. Single-surface high-wing pusher engine monoplane with hybrid control. Empty weight 160 lbs. Structural strength +7 Gs and -4 Gs.
![Page 65: Ultralight Aircraft](https://reader035.fdocuments.net/reader035/viewer/2022081415/558366f1d8b42a9c2b8b4b65/html5/thumbnails/65.jpg)
Lazair IV (1978)Lazair IV (1978)
Designed by Dale Kramer. Twin engine. Double surface wings produce 12:1 glide ratio. Estimated build time of 150 hrs. Empty weight 210 lbs.
![Page 66: Ultralight Aircraft](https://reader035.fdocuments.net/reader035/viewer/2022081415/558366f1d8b42a9c2b8b4b65/html5/thumbnails/66.jpg)
Lucky Stars II (2009)Lucky Stars II (2009)
A Mark Stull design. Empty weight 245 lbs. Payload 255 lbs. 60 mph cruise with a stall speed of 28 mph and rate of climb 600 fpm.
![Page 67: Ultralight Aircraft](https://reader035.fdocuments.net/reader035/viewer/2022081415/558366f1d8b42a9c2b8b4b65/html5/thumbnails/67.jpg)
Meadowlark (1984)Meadowlark (1984)
Designed by Jim Higgs. Empty weight 251 lbs. Structural limits +3.8 Gs and -1.5 Gs. Glide ratio 8:1.
![Page 68: Ultralight Aircraft](https://reader035.fdocuments.net/reader035/viewer/2022081415/558366f1d8b42a9c2b8b4b65/html5/thumbnails/68.jpg)
MirageMirage
Designed by Frank Riley. Aluminum tube and sailcloth with tractor engine. Empty weight 246 lbs. Payload 254 lbs. Structural limits +5.6 Gs and -2.8 Gs.
![Page 69: Ultralight Aircraft](https://reader035.fdocuments.net/reader035/viewer/2022081415/558366f1d8b42a9c2b8b4b65/html5/thumbnails/69.jpg)
Nomad/HonchoNomad/Honcho
Single seat, pusher engine high wing monoplane. Aluminum tube and sailcloth covering.Empty weight 189 lbs. Build time 120-150 hrs.
![Page 70: Ultralight Aircraft](https://reader035.fdocuments.net/reader035/viewer/2022081415/558366f1d8b42a9c2b8b4b65/html5/thumbnails/70.jpg)
Mono-FlyMono-Fly
Bob Teman's design known for its toughness. Aluminum, steel and composite construction. Structural limits +10 Gs and -10 Gs. Empty weight 250 lbs. Payload 300 lbs.
![Page 71: Ultralight Aircraft](https://reader035.fdocuments.net/reader035/viewer/2022081415/558366f1d8b42a9c2b8b4b65/html5/thumbnails/71.jpg)
Motor BipeMotor Bipe
Empty weight 225 lbs. Cruise speed 60 mph and stalls at 26 mph. Climb rate 750 fpm. Estimated build time of 175 hrs.
![Page 72: Ultralight Aircraft](https://reader035.fdocuments.net/reader035/viewer/2022081415/558366f1d8b42a9c2b8b4b65/html5/thumbnails/72.jpg)
Nova-1 (2007)Nova-1 (2007)
Designed by Gerald Nelson. Mid-wing monoplane of composite materials. Cruise speed 55 mph and stalls at 25 mph with a climb rate of about 500 fpm.
![Page 73: Ultralight Aircraft](https://reader035.fdocuments.net/reader035/viewer/2022081415/558366f1d8b42a9c2b8b4b65/html5/thumbnails/73.jpg)
P-38 LightningP-38 Lightning
Designed by Jim Mead. Twin boom fuselages. Wood, tube and fabric construction. Structural limits +4 Gs and -4 Gs. Glide ratio 7:1. Empty weight 305 lbs
![Page 74: Ultralight Aircraft](https://reader035.fdocuments.net/reader035/viewer/2022081415/558366f1d8b42a9c2b8b4b65/html5/thumbnails/74.jpg)
PapillonPapillon
Designed by D. Paup. 22 hp Polaris snowmobile engine. Empty weight 189 lbs. Cruise speed 30 mph and stalls at approx. 24 mph.
![Page 75: Ultralight Aircraft](https://reader035.fdocuments.net/reader035/viewer/2022081415/558366f1d8b42a9c2b8b4b65/html5/thumbnails/75.jpg)
P-CraftP-Craft
Designed by D. Paup. 2-axis control with pusher engine. Empty weight 165 lbs. Payload 237 lbs. Cruise speed 50 mph and stall speed 22 mph. Rate of climb 300 fpm.
![Page 76: Ultralight Aircraft](https://reader035.fdocuments.net/reader035/viewer/2022081415/558366f1d8b42a9c2b8b4b65/html5/thumbnails/76.jpg)
PDQ-2 (1973)PDQ-2 (1973)
.The PDQ-2 was designed by Wayne Ison. Empty weight 218 lbs. Cruise speed 70 mph and stall speed 46 mph. Rate of Climb 400 fpm. Rockwell JLO engine.
![Page 77: Ultralight Aircraft](https://reader035.fdocuments.net/reader035/viewer/2022081415/558366f1d8b42a9c2b8b4b65/html5/thumbnails/77.jpg)
Penetrater (1985)Penetrater (1985)
Pilot flies prone. Empty weight 175 lbs. Cruise speed 60 mph and stall speed 24 mph. Structural limits +6 Gs and -6 Gs. Glide ratio 14:1. 40 hr build time
![Page 78: Ultralight Aircraft](https://reader035.fdocuments.net/reader035/viewer/2022081415/558366f1d8b42a9c2b8b4b65/html5/thumbnails/78.jpg)
PinocchioPinocchio
Resembles Fokker Eindecker from WWI. Estimated build time 750 hrs. 45 hp 1/2 /VW engine. Cruise speed 55 mph and stall speed 27 mph. Climb Rate 750 fpm. Empty weight 254 lbs.
![Page 79: Ultralight Aircraft](https://reader035.fdocuments.net/reader035/viewer/2022081415/558366f1d8b42a9c2b8b4b65/html5/thumbnails/79.jpg)
Pioneer FlightStarPioneer FlightStar
Cruise speed approx. 50 mph. Stalls at approx. 25 mph. Structural limits are +6 Gs and -4 Gs. Empty weight 247 lbs. Payload 253 lbs.
![Page 80: Ultralight Aircraft](https://reader035.fdocuments.net/reader035/viewer/2022081415/558366f1d8b42a9c2b8b4b65/html5/thumbnails/80.jpg)
Poorboy PB-1Poorboy PB-1
Single-seat, high-wing, monoplane. Empty weight 254 lbs. Build time 450 hrs. Plans only
![Page 81: Ultralight Aircraft](https://reader035.fdocuments.net/reader035/viewer/2022081415/558366f1d8b42a9c2b8b4b65/html5/thumbnails/81.jpg)
P.U.P. (1983)P.U.P. (1983)
(Perfect Ultralight Plane). Designed by Lyle Matthews and sold as plans. Cruise speed 40 mph, stall speed 28 mph. Climb rate 600 fpm. Empty weight 248 lbs.
![Page 82: Ultralight Aircraft](https://reader035.fdocuments.net/reader035/viewer/2022081415/558366f1d8b42a9c2b8b4b65/html5/thumbnails/82.jpg)
Quicksilver MX Sprint (1981)Quicksilver MX Sprint (1981)
Designed by Dave Cronk. Empty weight 250 lbs. Load factors +5 Gs -3 Gs. Cruise speed 46 mph, stall speed 24 mph. Assembly time estimated at 30 to 40 hrs.
![Page 83: Ultralight Aircraft](https://reader035.fdocuments.net/reader035/viewer/2022081415/558366f1d8b42a9c2b8b4b65/html5/thumbnails/83.jpg)
Rally SportRally Sport
Designed by Bill Adaska. Empty weight 248 lbs. Structural limits +6 Gs and -3 Gs. 6. Glide ratio 8:1.
![Page 84: Ultralight Aircraft](https://reader035.fdocuments.net/reader035/viewer/2022081415/558366f1d8b42a9c2b8b4b65/html5/thumbnails/84.jpg)
Sandpiper ULS (1983)Sandpiper ULS (1983)
Designed by R.N. Miller. Original wing covered by balloon-type heat shrink fabric. Approx. build time 120 hrs. Structural limits are +6 Gs and -4 Gs. Empty weight 254 lbs.
![Page 85: Ultralight Aircraft](https://reader035.fdocuments.net/reader035/viewer/2022081415/558366f1d8b42a9c2b8b4b65/html5/thumbnails/85.jpg)
Sadler VampireSadler Vampire
The first aircraft Mr. Sadler produced was all metal. Cruise speed 63 mph, stall speed 25 mph. Empty weight 245, payload 250 lbs, Structural limits +6 Gs and – 6 Gs.
![Page 86: Ultralight Aircraft](https://reader035.fdocuments.net/reader035/viewer/2022081415/558366f1d8b42a9c2b8b4b65/html5/thumbnails/86.jpg)
Skybaby (1983)Skybaby (1983)
Single seat, pusher aircraft. Wood, tube and fabric construction. Empty weight 155 lbs. Payload 205 lbs. Structural limits +5 Gs and -3 Gs.
![Page 87: Ultralight Aircraft](https://reader035.fdocuments.net/reader035/viewer/2022081415/558366f1d8b42a9c2b8b4b65/html5/thumbnails/87.jpg)
Skycycle (1984)Skycycle (1984)
Single seat, parasol-wing monoplane. Empty weight 254 lbs. Payload 200 lbs. Load factors +3.5 Gs and -2 Gs. Cruise speed 40 mph, stall speed 27 mph. Climb rate 500 fpm.
![Page 88: Ultralight Aircraft](https://reader035.fdocuments.net/reader035/viewer/2022081415/558366f1d8b42a9c2b8b4b65/html5/thumbnails/88.jpg)
Snoop I (1981)Snoop I (1981)
Designed by Bob Able. Stall speed 18 mph. Empty weight 238 lbs. Payload 280 lbs. Structural limits +6 Gs and -4 Gs.
![Page 89: Ultralight Aircraft](https://reader035.fdocuments.net/reader035/viewer/2022081415/558366f1d8b42a9c2b8b4b65/html5/thumbnails/89.jpg)
Sparrow (1987)Sparrow (1987)
Single place, hi-wing monoplane. Empty weight 254 lbs. Payload 250 lbs. Cruise speed 58 mph and stall speed 26 mph. Climb rate 750 fpm.
![Page 90: Ultralight Aircraft](https://reader035.fdocuments.net/reader035/viewer/2022081415/558366f1d8b42a9c2b8b4b65/html5/thumbnails/90.jpg)
Stratos (1982)Stratos (1982)
Designed by Larry Burke. Cruise speed 63 mph, stall speed 27 mph. Climb rate 750 fpm. Load factors +6 Gs and -3 Gs. Empty weight 250 lbs.
![Page 91: Ultralight Aircraft](https://reader035.fdocuments.net/reader035/viewer/2022081415/558366f1d8b42a9c2b8b4b65/html5/thumbnails/91.jpg)
SunbirdSunbird
Developed by John W. Tucker. Cruise speed 40 mph, stall speed 20 mph. Climb rate 450 fpm. Empty weigh 250 lbs. Payload 275 lbs. Load factors +3 Gs and -3 Gs.
![Page 92: Ultralight Aircraft](https://reader035.fdocuments.net/reader035/viewer/2022081415/558366f1d8b42a9c2b8b4b65/html5/thumbnails/92.jpg)
Stinger S-17Stinger S-17
Covering is thermo-retractable sailcloth. Approximate build time 120-250 hrs. Cruise speed 55 mph, stall speed 27 mph and climb rate 800 fpm. Empty weight 250 lbs. Payload 317 lbs.
![Page 93: Ultralight Aircraft](https://reader035.fdocuments.net/reader035/viewer/2022081415/558366f1d8b42a9c2b8b4b65/html5/thumbnails/93.jpg)
SunburstSunburst
Designed by John Massey. 30 hp. engine. Breaks down to fit in a storage bag. Cruising speed 35 mph, stalling speed 25 mph, climb rate 800 fpm. Empty weight 253 lbs. Estimated 30 hr. construction time.
![Page 94: Ultralight Aircraft](https://reader035.fdocuments.net/reader035/viewer/2022081415/558366f1d8b42a9c2b8b4b65/html5/thumbnails/94.jpg)
Tristar (1980)Tristar (1980)
A Dick Turner design. Cruise speed 45 mph, stall speed 21 mph. Climb rate 800 fpm. Empty weight 200 lbs. Structural limits +5.8 Gs and -3 Gs.
![Page 95: Ultralight Aircraft](https://reader035.fdocuments.net/reader035/viewer/2022081415/558366f1d8b42a9c2b8b4b65/html5/thumbnails/95.jpg)
UltrastarUltrastar
Designed by Homer Kolb. Steel tube and fabric construction. 3-Axis control system. Empty weight 235 lbs.
![Page 96: Ultralight Aircraft](https://reader035.fdocuments.net/reader035/viewer/2022081415/558366f1d8b42a9c2b8b4b65/html5/thumbnails/96.jpg)
Vector 600Vector 600
Designed by Berndt Petterson, Mike McCarron and Paul Yarnell. 22 hp engine. Cruise speed 45 mph with stall at 26 mph. Climb rate 600 fpm. Empty weight 195 lbs. Structural limits +5.7 Gs and -2.8 Gs.
![Page 97: Ultralight Aircraft](https://reader035.fdocuments.net/reader035/viewer/2022081415/558366f1d8b42a9c2b8b4b65/html5/thumbnails/97.jpg)
Viking (1983)Viking (1983)
Designed by Kevin Bell. 38 hp engine. Cruise speed 45 mph and stall speed 23 mph. Climb rate 800 fpm. Requires 75-100 hrs. for construction. Empty weight 244 lbs. Useful load 225 lbs. Structural limits +5 Gs and -3 Gs.
![Page 98: Ultralight Aircraft](https://reader035.fdocuments.net/reader035/viewer/2022081415/558366f1d8b42a9c2b8b4b65/html5/thumbnails/98.jpg)
Viper IIViper II
Aluminum tube and Dacron covered wing. Twin tailbooms. Empty weight 150 lbs.
![Page 99: Ultralight Aircraft](https://reader035.fdocuments.net/reader035/viewer/2022081415/558366f1d8b42a9c2b8b4b65/html5/thumbnails/99.jpg)
Weedhopper (1977)Weedhopper (1977)
2-Axis control with tricycle landing gear. Empty weight 250 lbs. Payload 300 lbs. Cruise speed 55 mph and stall speed 20 mph. Rate of climb 1000 fpm.
![Page 100: Ultralight Aircraft](https://reader035.fdocuments.net/reader035/viewer/2022081415/558366f1d8b42a9c2b8b4b65/html5/thumbnails/100.jpg)
Whing Ding II (1971)Whing Ding II (1971) Designed by Bob Hovey.
Essentially a plywood box filled with urethane foam. 14 hp McCulloch chainsaw engine. Cruise speed 40 mph, stall speed 26 mph, climb 100 fpm. Empty weight 123 lbs. Construction time around 400 hrs.
![Page 101: Ultralight Aircraft](https://reader035.fdocuments.net/reader035/viewer/2022081415/558366f1d8b42a9c2b8b4b65/html5/thumbnails/101.jpg)
Witch (1982)Witch (1982) Designed by Marvin
Greenwood. Easily transportable. 22 hp engine. Cruise speed 50 mph, stalling speed 26 mph. Structural limits +3.8 Gs and -2 Gs.
![Page 102: Ultralight Aircraft](https://reader035.fdocuments.net/reader035/viewer/2022081415/558366f1d8b42a9c2b8b4b65/html5/thumbnails/102.jpg)
Wizard 1Wizard 1
Weight shift control system. Single surface, wire braced wing. Empty weight 167 lbs. Approximate build time 100 hrs. Glide ratio 9:1.
![Page 103: Ultralight Aircraft](https://reader035.fdocuments.net/reader035/viewer/2022081415/558366f1d8b42a9c2b8b4b65/html5/thumbnails/103.jpg)
WoodhopperWoodhopperDesigned by John Chotia and featured on Popular Mechanics cover in 1978. Empty weight 145 lbs. Maximum pilot weight 200 lbs. Stress limit +3.5 Gs. Construction time 250-300 hrs.
![Page 104: Ultralight Aircraft](https://reader035.fdocuments.net/reader035/viewer/2022081415/558366f1d8b42a9c2b8b4b65/html5/thumbnails/104.jpg)
Wren (1982)Wren (1982)
Designed by Mark Calder. Composite construction with Dacron covering. 28 hp 440A engine standard. Empty weight 241 lbs. Kit or plans built.
![Page 105: Ultralight Aircraft](https://reader035.fdocuments.net/reader035/viewer/2022081415/558366f1d8b42a9c2b8b4b65/html5/thumbnails/105.jpg)
ZingZingDesigned by Scott Lane. Estimated build time is 300-500 hrs. 30 hp Kawasaki engine. Cruise speed 60 mph and stall speed 27 mph. Climb rate 650 fpm. Empty weight 249 lbs. Payload 250 lbs.
![Page 106: Ultralight Aircraft](https://reader035.fdocuments.net/reader035/viewer/2022081415/558366f1d8b42a9c2b8b4b65/html5/thumbnails/106.jpg)
More information can be viewed at virtualultralightmuseum.com.
Over 300 aircraft, from all over the world, are included with pictures and comprehensive descriptions.
VUM, 03/2011VUM, 03/2011