Cab Wasp Cadet Cadet MkIII Calypso CGS Hawk Challenger I Chandelle MkIV Chickenox Chinook WTR-11 Citizen Fly Clipper Cloudbuster Cloud Dancer Cloudhopper MkII Cloudrider Cloudster I Cobra Condor II Condor (Cohen) Connie Coyote Cumulus Cygnet
Cab Wasp. (Aus). Late 70s design. Fuji Robyn 250 cc, one cycle engine with belt drive. Similar to the Wheeler Scout Mk2, but
with strut braced wing.
Cadet. Tractor
engine. Aluminum tube and sailcloth construction. 3-Axis with yoke control.
Roll uses half-span ailerons. Double surface and strut braced wing. Tricycle
landing gear with steerable front wheel. Length 16.5', height 8', wing span
30', wing area 163 sq/ft. Empty weight
Cadet Mk III Motor Tutor.
A single seat, high wing, open cockpit aircraft,
V.W. powered (1500-1600 cc.), using
Calypso.
(1984). 3-axis controls. Full-span
ailerons. Tricycle landing gear with steerable nose wheel. True tapered
wings. Double surface wings. Parachute standard equipment. L 19, h6.6,
Wing span
CGS
Hawk. (U.S., 1981).
Conceived by Chuck Slusarczyk. Length 20.7, height 6/89, wing span
28.8, wing area 135 sq/ft. Empty weight
Challenger I. 3-Axis
with full-span ailerons. Steerable nosewheel. Double surface wings and
enclosed cockpit with optional doors. Factory built airframe and wings. Dope
and fabric covering. Estimated 100 hours build time. Length 18.5, height
6. Empty weight 235 lbs. Payload 265 lbs. Wing span 31.5 ft. Wing area 142
sq/ft. Load factors +4 Gs and -3 Gs. Glide ratio 10:1.
Quad City UL,
Chandelle Mk IV. Designed by Nile Downer. Sing-seat high-wing monoplane with three-axis control. Tricycle landing gear. Aluminum alloy tube airframe. Single surface wing. Wing span 30.3, wing area 176 sq/ft. Empty weight 243 lbs. Payload 257 lbs. 35 hp Cuyuna ULII-02 pusher engine. Climb rate 650 fpm. Cruise speed 40 mph and stall speed 22 mph. Chandelle Aircraft.
Chickinox Monoplace. (Belg, 1984). Designed by Jacky Tonet. 2-Axis control. Stainless steel tubular structure. Length 16.4, height 7.2, wing span 30.8, wing area 142 sq. Empty weight 289 lbs, Payload 218 lbs. +6 Gs and -3 Gs. Glide ratio 10:1. Dynali SA.
Chinook WT-11.
(Can. 1977). Single seat, enclosed cockpit with pusher engine. Designed by
Wladymir Talanchuk and Curt Lumas. Aluminum tube and sailcloth construction.
3-Axis controls. Hi-wing, double surface, strut braced wing. Taildragger
with steerable tailwheel. Length 17.6', height 5'11", wing span
35'.Structural limits +5.5 Gs and -3 Gs. Glide ratio 10:1. Empty weight
Citizen Fly.
Single seat,
pusher engine hi-wing monoplane. Length 18', height 5.1'. Wing span 27',
wing area 100 sq/ft. Empty weight
Clipper.
(1984).
Designed by Fred Bell and re-introduced in 2002. Single
seat parasol, strut braced, high wing taildragger aircraft with a tractor
engine. Uses a 4130 chromoly welded steel fuselage with double surfaced
wings covered with dacron sailcloth.
Wing span
Cloudbuster
(1981). Powered
glider with tractor engine, Aluminum, fabric and composite construction.
3-Axis controls. Double surface, strut braced tapered wings with half-span
ailerons. Tricycle landing gear with steerable nosewheel. Length 15.6,
height 7.4, wing span
Cloud Dancer. (1983).
Pusher type V-tail powered glider designed by Erwin Rodger and Delura Roger.
Aluminum tube and sailcloth construction. 80% double surface cantilever
wings. Taildragger with steerable tail wheel. 3-Axis control uses
ruddervators and spoilerons. Construction is aluminum tube, and dacron sail
cloth. Length 17, height 4.5, Wing span 40', wing area 132 sq/ft. Empty
weight
Cloudhopper MkII.
(Brit.) Singe-seat, strut braced, high wing monoplane. 2-Axis control system
with tricycle landing gear. Steerable nosewheel. Tube and Dacron design.
Empty weight
Cloud Rider.
Low front mounted engine with tricycle landing
gear and strut braced double surface wing. 3-axis control.
Cloudster I.
Introduced at Oshkosh 1996 and first flew in
1999. Wood with metal struts. The plane was available in plans or as sub
component kits. 3-Axis controls with tail dragger configuration with pilots
legs extended outside the fuselage to the rudder pedals. Length 16.4, wing
span
Cobra. (U.S.
1982). Designed by Wayne and Kerry Richter. Single seat monoplane with
pusher engine configuration. Conventional 3-Axis control. Double surface
wire braced wing with spoilerons. Tricycle landing gear with optional
steerable front wheel and nosewheel brakes. 30 hp 430RR Cuyuna engine.
Cruise speed
Condor.
Designed by Buddy Head, Bob Carswell and Dave French. Single seat with
pusher engine. Aluminum tube and sailcloth construction. 3-Axis controls.
Single surface wire braced wings with spoilers. Tricycle landing gear.
Non-steerable nosewheel. Kawasaki 440 engine. Climb rate 775 fpm. Length
10', height 9.7', wing span 32', wing area
Condor. Designed by Steve Cohen as a second generation refined version of the Stolaero.
Connie.
The Connie is an amphibious single center float ultralight, with wing tip
floats on the wings. The pilot sits in front of the wing, in a seat on top
of the float. The Connie uses bolt and rivet together construction, covered
in Dacron sail cloth, with estimated building times in the 100 hour range.
Empty weight
Coyote. Designed by Randy Schlitter as a single-seat high-wing monoplane. Conventional 3-axis controls. Wing braced by cables and kingpost. Fuselage and empennage covered. Semi-enclosed cockpit. Taildragger with optional brakes. Length 17, height 5.5. Wing span 32, wing area 133 sq/ft. 28 hp Rotax 277 tractor engine. Empty weight 249 lbs, payload 286 lbs. Load factors +3.5 Gs and -1.5 Gs. Cruise speed 40 mph, stall speed 25 mph. Glide ratio 10:1. Rans Inc., Hays, Ks.
Cumulus. (
Cygnet. Pamco. According to Steve Robards the Cygnet was built in S.E. Queensland around 1981/1982. It had a welded airframe and aluminum wings. (No specs available).
