Nieuport 11 ultralight, Nieuport 11 ultralight aircraft, Graham Lee Nieuport 11 WW1 replica fighter ultralight aircraft kit.

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Graham Lee Nieuport 11 WW1 replica fighter ultralight aircraft kit.

Started in 1984 with the design and prototyping of a 7/8 scale Nieuport 11 carrying Canadian ultra light registration C-IRCA.
The single seat Nieuport was 4 months in design and construction, and preparation of the plans took another 6 months of full time effort.
The Canadian Ultra light was 12 pounds over the U.S. ultra light weight limit, which placed it in the U.S. experimental category; and with a little change in engine and tube sizes also allowed it to be built as a U.S. ultra light.

Wing Span
 21.50 ft. 
Range
 165 sm 
Wing Area
 114.0 sq. ft.
Takeoff Dist .
160 ft. 
Length
16.50 ft, 
Landing Dist .
275 ft. 
Max Gross Wt .
550 lbs. 
VNE
 83 mph 
Empty Wt .
250 lbs.
Cruise
 65 mph 
Payload (full fuel) 200 lbs.  Stall
 27 mph 
Fuel Capacity
 12 gal. 
Climb Rate @msl
 750 fpm 
Seats 1  Service Ceiling 15,000 ft. 
Cabin Width
24 in. 
 
Engine  

30-50 hp 

Construction aluminum tubing
Plans Available Est. Bldg. Time  700 hrs. I

Graham Lee
Box 889
Lamont Alberta
T0B 2R0 Canada

As of May, 2000 more than 1250 sets of Nieuport 11 plans in circulation, and at least 100 examples have flown successfully, in Canada, the U.S., Brazil, Argentina, New Zealand, Australia, Japan, South Africa, Czech Republic, Finland, Germany, Italy, France, and Spain.

In 1989, Graham designed and built the 2 place Nieuport 12 prototype, registered C-GXII as a Canadian Amateur built. (exp. in the U.S.) With it's debut at Oshkosh '90, the prototype was awarded runner up in the Experimental category (3rd place); an astonishing accomplishment for a prototype, and a credit to the finishing work of the planes owner, Bob Robertson.
There are 6 flying examples, as of July '97, and several nearing completion, from a total of 77 sets of plans in circulation.

Since their conception, neither model has required a design change, and both models have been built and flown successfully at well over the design gross.

In 1999 the Nieuport Bebe was up-sized to include FULL SIZE for taller folks; and 2000 brings a BRAND NEW design.
MIRANDA is a conventional gear, single seat, closed cabin, stagger wing, sesqui-plane (with a small wing below like the Nieuport).
At under 300 pounds empty and 650 pounds gross, MIRANDA is designed as a high speed S.T.O.L. aircraft without levers and gadgets to be forgotten.
The unique Whittman wing tip actually enhances both ends of the speed range, and does it with less work and less materials than a conventional wing tip!
The sesqui-wing arrangement with 1/4 LESS wing area has been proven to out perform other bi-plane styles, in climb, manoeuverability, ceiling and top speed.
MIRANDA broadens the ENTIRE flight envelope, with LESS materials and work.

Prior to producing the Nieuport designs for the "home built" market; in reverse order, Graham designed and built a 2 place Petit's Breezy UL; contributed to the design of the Birdman Chinook WT11 and designed the production tooling. designed the Birdman Atlas X-C, and prepared tooling, prototypes, production drawings and assembly manuals for the early Birdman Enterprises Ultra light aircraft.

Before involvement with that company, Graham assisted in production and kit assembly with the Canadian representative of the KR-1 and KR-2 and built a Bensen B-8M. Graham holds EAA membership # 113519

While admittedly a bit rusty, Graham is a journeyman machinist, toolmaker, auto mechanic, motorcycle mechanic and automotive machinist, More recently, a designer, writer, publisher and inventor in automotive and electrical fields.

The above  can be found at: http://plaza.powersurfr.com/circa/

Circa Reproductions Inc.
46 New Brighton Circle SE
Calgary, Alberta
http://www.nieuports.com/
 

Nieuport 11 ultralight aircraft

For several web video interviews on the Nieuport 11 subscribe to the Ultralight Flyer web video magazine.
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