Clement-Bayard

Adolphe Clément-Bayard circa 1907

Clément-Bayard was a French manufacturer of automobiles, aeroplanes and airships founded in 1903 by the entrepreneur Adolphe Clément-Bayard (née Adolphe Clément). The name celebrated the Chevalier Pierre Terrail, seigneur de Bayard who saved the town of Mézières in 1521. A statue of the Chevalier stood in front of the Mézières factory, and the image was incorporated into the company logo.

In 1894 he started construction work on a former military site in the Faubourg Saint-Julian at Mézières, to build a new factory, which would become known as La Macérienne. Clément personally supervised the work remotely using photographs taken every day and visiting the site once a week. By 1897 it was producing components and spokes for the Gladiator Cycle Company. It covered 15,000 sq.m and using a hydraulic turbine power plant, a steam room, large machine hall, a foundry, a workshop for the nickel processing, the operation with the manufacturing of nuts and spokes on a bike. The factory building still exists but in the spring of 2006 it was transformed into a cultural center.

From 1903 Clément-Bayard automobiles were built in a ‘state of the art’ factory at Mézières, known as La Macérienne, which Clément had designed in 1894 mainly for building bicycles.

In 1908 ‘Astra Clément-Bayard’ began manufacturing airships at a new factory in La Motte-Breuil in response to a French Army decision to commence airship operations. Seven Clément-Bayard airships were completed.

Aircraft test flights began in 1908 and Louis Capazza’s ‘planeur (glider) Clément-Bayard’ was unveiled in L’Aérophile on 15 May 1908. Clement-Bayard was pioneer of welded steel tube airframe construction. Clément-Bayard also built Alberto Santos-Dumont’s Demoiselle No 19 monoplane that he had designed to compete for the Coupe d’Aviation Ernest Archdeacon prize from the Aéro-Club de France. The plane was small and stable, but they planned a production run of 100 units, built 50 and sold only 15 for 7,500 francs for each airframe. It was the world’s first series production aircraft. By 1909 it was offered with a choice of 3 engines, Clement 20 hp; Wright 4-cyl 30 hp (Clement-Bayard had the license to manufacture Wright engines); and Clement-Bayard 40 hp designed by Pierre Clerget. It achieved 120 km/h.

Pierre Clerget designed a range of Clement-Bayard aircraft engines including a 7-cylinder supercharged radial, the 4-cyl 40 hp used on the Demoiselle, a 4-cyl 100 hp used on ‘Hanriot Etrich’ monoplanes, and a V8 200 hp airship engine. By 1909 Clement-Bayard had the license to manufacture Wright engines alongside their own design.

Circa 1909 Adolphe Clément received permission from the Conseil d’État to change his name to Adolphe Clément-Bayard.

In 1910 the Clement-Bayard Monoplane No. 1 was introduced at the Paris show.

By 1912 Clément-Bayard built a biplane plus three different models of horizontally opposed aircraft engines.

In November 1912 the Clement-Bayard Monoplane No. 5 was introduced. It was powered by a Gnome 7-cylinder rotary engine producing 70 hp (52 kW). The pilot sat in an aluminium-and-leather tub.

Gnome-engined Clement-Bayard two-seat monoplane set world distance record of 255 miles (410 km) February 1913. Same year other Gnome-engined civil/military monoplanes appeared.

In 1913 a three-seater biplane was introduced as part of the military project, the Clement-Bayard No. 6. It was configured for two observers in front of the pilot, and was powered by either a 4-cyl 100 hp (75 kW) Clement-Bayard or 4-cylinder Gnome engine.

At Olympia Aero Show, London, March 1914, exhibited an all-steel armored monoplane. Clément-Bayard produced a steel scouting monoplane powered by either an 80 hp (60 kW) motor or a 100 hp (75 kW) Gnome et Rhône engine. The nickel steel armour was designed for protection against rifle fire.

Adolphe Clément ceded control of Clément-Bayard to his son Maurice in early 1914, but the consequences of World War I for the company were disastrous. The La Macérienne factory at Mézières was lost to the Germans, the machinery was shipped back to Germany, and the forges, foundries and smelter were destroyed. The gutted building was used as an indoor riding school for German officers.

Automobile production in Levallois-Perret, Paris, was suspended as the factory was turned over to war production, military equipment and military vehicles, aero engines, airships and planes.

In 1922 the Clément-Bayard automobile company was sold to André Citroën, in whom Adolphe Clément also invested financially, and the factory at Levallois-Perret became the centre of 2CV manufacturing for the next 40 years.

In 1922 the company was broken up and the factory in Paris was taken over by Citroën. In 1928 Clement-Bayard sold his factory to Citroen.

Cleary CL-1 Zipper

Single-seat light aircraft with twin booms and pusher propeller, designed and built by Laister Sailplanes and first flown 1983.

The CL-1 was powered with a 38 hp Kawasaki engine and had a power off glide ratio of 18-1.

The Zipper was first registered in 1983 as N3999C Serial Number X1.

I worked in building this aircraft with Jack Laister for Bill Cleary. Jack was the Engineer and I was the A&P. I’m trying to locate where this aircraft is. Both Jack and Bill have passed on now.
Timothy Blackmon

Classic Sport Aircraft S-18 / S-18T

John Thorp retired in 1985 and took the T-18 plans off the market. Lu Sunderland, having worked with John on a wider fuselage and folding wing option for the T-18, did a complete rework of the drawings and produced plans for the S-18. The S-18 is then a redesign of the Thorp T-18. The fuselage body is 2″ wider and 5″ longer than the standard T-18. Also it has a newer NASA computer designed Wing Airfoil, which is stated to lower the stall speed by 6-8 knots. This airfoil also allows a more gentle stall with adequate warning. The top and cruise speeds remain the same. An S-18 with an 160hp Lycoming IO-320 and Hartzel Constant Speed propeller will cruise around 180 mph at 8500 ft (MSL) on less than 7 GPH (gallons per hour of fuel).
The S-18, like the T-18 is an all metal 2 place side-by-side high performance aircraft. Control response is exceptional and control forces are well harmonized. The S-18 is a very capable cross-country airplane. It will carry 2 people and 80 lbs. of baggage. Powerplants range from Lycoming O-235 (115hp) to IO-360 (180).
Parts can be provided with matched holes so that parts fit together saving a lot of time in construction. Also parts are scribed to outer mold-lines or trim lines. No jigs are required. The airplane is built using 1/8″ solid aluminum rivets, but can be built using 1/8″ stainless steel pop rivets (but not recommended).
The S-18 has a folding wing designed by Lu Sunderland which can be swung around parallel to the fuselage making the airplane less than 8 feet wide. So that it can be trailered home or stored in small spaces.
Test Flights were completed on the S-18T Tri-Gear in May of 2003.

The S-18 was available in kit form from Classic Sport Aircraft. Pieces and parts for both the T-18 and the S-18 are available here also.

S-18T
Engine: Lycoming O-360
Propeller: constant speed
Wingspan 20′ 10″
Length 18′ 6″
Wing area: 86 sq.ft
Gross Weight 1600 lbs.
Empty Weight 1000 lbs.
Useful Load 600 lbs.
Fuel – Standard Tank 29 gallons
Fuel – Wing Tank 24 gallons
Rate of Climb 1500 fpm
Luggage Capacity 80 lbs.
Range (standard) 540 SM
Range (with optional wing tanks) 900 SM
Cruise – 75% power 180 mph
Top Speed 200 mph
Stall: 63 mph
Cockpit width; 40 in
Seating 2 side by side
Engine options: Lycoming 290, 320, or 360

Classic Fighter Industries

The first effort to make Me 262 copies, which began in the early 1990s and involved warbird fan Stephen L. Snyder and a Texas aircraft restoration company, Classic Fighter Industries, dissolved in acrimony. Snyder called on Bob Hammer to take over the work. The effort was barely under way when Snyder died in the crash of his North American F-86 jet fighter in 1999.

The aircraft were taken over by the Texas Aircraft Factory.

Classic Aviation Designs CA18

CA18-1320

The CA18-1320 is the lightest weight version. It is designed for New Zealand’s CAA Class Two Microlight category with a maximum all up weight of 600Kgs.

The basic aircraft does not come equipped with flaps or large grass all terrain tyres to keep weight to a minimum. Fuel is limited in each wing tank to 35 litres.

For this model you can choose between a full size J3 or PA18 Cub. The added bonus is that solo flight is from the front seat.

The CA18-1530 model is based on the 100hp Cub. With its 1530 MAUW capacity this model is suited for engines up to 120hp. To accommodate the increased weight capacity from the CA18-1320 model, it has increased size of the timber framework within the fuselage. The wings are the same, however the wing lift struts are larger and 50 litre fuel tanks are fitted.

Extra options available for the CA18-1530 model include:

  • Flaps
  • Larger main landing gear tries & rim kits for disc brake mounts
  • Large tail wheel assembly
  • Navagation and runway lighting kit

The CA18-1920 model is based on a 180hp retro fitted PA18 Super Cub. The CA18-1920 has a maximum all up weight of 1920lbs. To accommodate the increased load capacity, the timber framework within the fuselage along with the wing spar caps have been increased in size.

This model is an ideal platform to fit a STOL kit for those shorter and rougher landing areas.

CADL was to be offering STOL components for this model by the end of 2016, the components were to include:

  • Fibre glass hoerner style wing tips
  • Carbon fibre leading edge coverings (to replace the plywood)
  • Carbon fibre wing ribs
  • Fowler flaps
  • Modified undercarriage

Gallery

CA18-1320
Engine: Continental 0-200 / Rotax 912, 100 hp
Wing span: 10.668 m / 35.0 ft
Wing Area: 15.80 sq/m / 178.5 ft
MAUW: 1320 lbs
Fuel Capacity: 2 x 35 lt
Total useable fuel: 68 lt
Fuel type: 100 LL Avgas/ MOGAS
Main Landing Gear Tires: 6.00 x 4
Tail Wheel: 2.50 x 4
Axles & Bearings: 1 – ¼ inch
Brakes: Matco MLG
Wing Loading: 43.92 kgs/m / 8.5 lbs/ft
Wheel Base: 5.059 m / 16 ft
Wheel Track: 1.879 m / 74 in
Main Wheels: 21×8.00×6, 18 psi
Tail Wheel: 2.80×4, 20 psi
Elevator Maximum up Deflection: 25⁰
Elevator Maximum Down Deflection: 15⁰
Elevator Trim Maximum up Deflection: 3⁰
Elevator Maximum Down Deflection: 4⁰
Rudder Defection Left & Right: 25⁰
Tail wheel defection before unlocks to 360deg: 22⁰
Aileron deflection: Up 18deg, Down 18deg
Maximum G: +4, -0
Service Ceiling: 13,500ft
Manoeuvring Speed: 85 mph
Maximum Cruise: 100 mph
Never Exceed (Vne): 120 mph
Rate of Climb: 524 fpm at 71 mph
Best Angle of Climb: 64 mph
Best Rate of Climb (Ratio): 1 to 9.4
Stall Speed: 38 mph

CA18-1530
Engine: Continental O-200, 100 hp
Prop: Omega 71 x 41
Wing span: 10.668 m / 35.0 ft
Wing Area: 15.80 sq/m / 178.5 ft
MTOW: 1530 lb
Wing Loading: 43.92 kgs/m / 8.5 lbs/ft
Fuel Capacity: 2 x 50 lt
Total useable fuel: 98 lt
Fuel: 100 LL Avgas
Main Landing Gear Tires: 21/8.00 x 4
Tail Wheel: 2.80 x 4
Axles & Bearings: 1 – ¼ inch
Brakes: Matco MLG
Wheel Base: 5.059 m / 16 ft
Wheel Track: 1.879 m / 74 in
Main Wheels: 21×8.00×6 18 psi
Tail Wheel: 2.80×4, 20 psi
Elevator Deflection: +25⁰ / -15⁰
Elevator Trim Deflection: +3⁰ / -4⁰
Rudder Defection Left & Right: 25⁰
Tail wheel defection before unlocks to 360deg: 22⁰
Aileron deflection: Up 18deg / Down 18deg
Maximum Flap Speed (Vfe): 85 Mph
Flap deflection: 15deg / 25deg / 40deg
TO to 50ft: 332-372m
Landing dist from 50ft: 104-106m
ROC: 505-644 fpm at 71 mph
Stall Speed Angle of Bank 0⁰: 42 mph
Stall Speed Angle of Bank 10⁰: 44 mph
Stall Speed Angle of Bank 20⁰: 45 mph
Stall Speed Angle of Bank 30⁰: 47 mph
Stall Speed Angle of Bank 40⁰: 50 mph
Stall Speed Angle of Bank 60⁰: 55 mph
Stall Speed Angle of Bank 90⁰: 62 mph
Manoeuvring (Va): 90 mph
Max cruise: 110 mph
Never exceed: 138 mph
Flight Load: +4.4 / -0
Max Endurance: 5 hr
Service Ceiling: 13,500 ft
Manoeuvring Speed: 90 Mph
Max Cruise: 110 Mph
Never Exceed (Vne): 138 Mph
MAUW: 1530 lb
Best Rate of Climb: 624 fpm at 71 Mph
Best Angle of Climb: 64 Mph
Rate of Climb Ratio: 1 to 9.4
Stall Speed: 39 Mph

CA18-1920
Engine: Lycoming O-320 / 360, 160 / 180 hp
Wing span: 10.668 m / 35.0 ft
Wing Area: 15.80 sq/m / 178.5 ft
Fuel Capacity: 2 x 50 lt
Total useable fuel: 98 lt
Fuel: 100 LL Avgas
Main Landing Gear Tires: 21/8.00 x 4
Tail Wheel: 2.80 x 4
Axles & Bearings: 1 – ¼ inch
Brakes: Matco MLG
Wheel Base: 5.059 m / 16 ft
Wheel Track: 1.879 m / 74 in
Main Wheels: 21×8.00×6 18 psi
Tail Wheel: 2.80×4, 20 psi
Wing Loading: 43.92 kgs/m / 8.5 lbs/ft
Wheel Base: 5.059 m / 16 ft
Wheel Track: 1.879 m / 74 in
Main Wheels: 21×8.00×6 18 psi
Tail Wheel: 2.80×4, 20 psi
Elevator Deflection: +25⁰ / -15⁰
Elevator Trim Deflection: +3⁰ / -4⁰
Rudder Defection Left & Right: 25⁰
Tail wheel defection before unlocks to 360deg: 22⁰
Aileron deflection: Up 18deg / Down 18deg
Maximum Flap Speed (Vfe): 85 Mph
Flap deflection: 15deg / 25deg / 40deg
Flight Load: +4.4 / -0
Service Ceiling: 13,500 ft
Manoeuvring Speed: 94 Mph
Max cruise: 110 mph
Never exceed: 138 mph
MAUW: 1920 lb
ROC: 980 fpm at 71 mph
Best Angle of Climb: 64 Mph
Rate of Climb Ratio: 1 to 9.4
Stall Speed: 42 Mph

Classic Aviation Designs Ltd

The concept of Classic Aviation Designs Limited was conceived in 2004, and the company was incorporated on 31 Janauary 2012. Originally the concept was to reintroduce affordable aviation at grassroot levels to new and experienced builders of aircraft.

Designing and building of the Adventurer CA18 was as a sideline. Part of the inspiration behind the Adventurer CA18 was to attract a new generation to sport flying and aviation related careers.

With the assistance of some key people such as Sid Siddiqi an ex Nasa engineer and retiree, CADL was able to present the concept of the Clubflyer Education Programme (CEP) at the 2011 and 2012 Oshkosh Trade Show. This concept was universally agreed, by all who attended the talks or from those spoken to privately at the event, that the programme had good merit to help revitalise the aging issues of aviation.

From the initial concept it was identified that private builders would also be interested in building the aircraft. CADL revised its initial education project to also incorporate a private builders programme.

Clark 1910 Multiplane

Invented by William R Clark, a mechanic from Spokane, Washington. It measured 52 ft x 63 ft and had a wing area of 2000 square feet. The monster flying machine was first revealed to the press in April 1910. The Western Motor Plane Company had been formed to help develop the flying machine, but by January 1911, it was being sued by unpaid creditors.