2008: Dcs, Inc.
12618 Millstream Drive
Bowie, Md 20715-1618 USA.
Airplane builder
2008: Dcs, Inc.
12618 Millstream Drive
Bowie, Md 20715-1618 USA.
Airplane builder

Appearing at the 1997 show at Blois the Termerair featres a fuselage in tube and fabric with laminated floats.
Engine: Rotax 582, 64 hp
Wing span: 10.50 m
Wing area: 16 sq.m
MAUW: 495 kg
Empty weight: 235 kg
Fuel capacity: 55 lt
Max speed: 140 kph
Cruise speed: 110 kph
Minimum speed: 60 kph
Climb rate: 3.5 m/s
Seats: 2
Fuel consumption: 12 lt/hr
Price (1998): 192,000 Fttc
1998:
249 route de Pegomas
F-06130 Grasse
France
LSA amphibian builder
Had a single wheel landing-gear.
Side-by-side two-seat (last rotary-engined design for U.S. Army)
In 1920 Milton C. Baumann designed the revolutionary RB Racer, with solid all-wood wing, totally enclosed cockpit and retractable landing gear linked to rod-operated leading and trailing-edge camber-changing flaps.

The Dayton-Wright Messenger biplane was designed by Oliver Thomas in 1918. It was powered by a 37-hp DePalma V-4 engine. Dayton-Wright hoped to get an Army contract. Failing that, it was planned to sell on the civil market, but only one was built.
Engine: 37-hp DePalma V-4
Span: 19 ft 3 in
Length: 17 ft 6 in
Empty weight: 476 lb
Loaded weight: 636 lb
Speed: 85 mph
USA.
Formed during First World War at Dayton, Ohio, for quantity aircraft production, with Orville Wright as consulting engineer. Built Liberty-engined DH-4 (the “Liberty plane”) and Standard J-1. In 1919 built a limousine version of DH- 4, single-seat Messenger, and also a three-seater. In 1920 Milton C. Baumann designed the revolutionary RB Racer, with solid all-wood wing, totally enclosed cockpit and retractable landing gear linked to rod-operated leading and trailing-edge camber-changing flaps. Built the USB-1, an Engineering Division redesign of the Bristol Fighter; 1921 twin-engined seaplane; side-by-side two-seat TR- 3 (last rotary-engined design for U.S. Army) and singlewheel landing-gear TR-5. In 1922 built Douglas DF-2. In 1923 the parent company, General Motors, abandoned aviation and dissolved Dayton-Wright; aeronautical work of the company taken over by Consolidated Aeronautics Inc.
The Dayton-Wright Company approached the USAAS to replace their World War 1-era Curtiss JN-4 “Jenny” series of trainers and was in turn asked to deliver three TA-3 models for evaluation. Though the design itself proved promising enough, the TA-3 (designated with an “A” for its air-cooled engine operation) was delivered by request with an uprated Le Rhone engine of 110 horsepower. Still further evaluation models were ordered, this time with the requested Wright-Hispano I V-8, 150 horsepower engine of increased power (designated TW-3 with the “W” standing for its water-cooled engine process) finally culminating in an official order by the USAAS.
Production rights for the trainer were secured by the newly-created Consolidated Aircraft Company (established by Reuben Fleet of the Gallaudet firm) as General Motors was reviewing their commitment to aircraft production in a post-war world and would eventually shut down operations at Dayton-Wright altogether. The TW-3 was delivered by 1923 and became the first notable variant of the “Trusty” production line.

The 1929 Dayton Grant featured steel cylinders with detachable aluminium heads, with bronze valve seats shrunk in the heads. There is a special tulip valve design of special steel, one exhaust valve and one intake valve per cylinder.
The aluminium alloy pistons have full floating hollow piston pins. The crankshaft is one piece, with five bearings.
Equipment was an instruction book, tool kit, and exhaust flanges.
Available at extra cost were C-5 fuel pump, hub for a wooden or steel propeller, and starter.
Type: 8 cylinder horizontal opposed
Military Rating: 225 hp at 1800 rpm
Commercial Rating: 240 hp at 2000 rpm
Displacement: 764 cu.in
Compression ratio: 5.3-1
Bore: 4 1/2 in
Stroke: 6 in
Length: 56 in
Width: 44 in
Height: 20 in
Weight: 500 lb
Fuel consumption: not more than 1.05 lb/hp/hr
Oil consumption: not more than .025 lb/hp/hr
Lubrication: Force feed
Ignition: Dual spark magneto or generator for battery ignition
Carburation: 2 Zenith or Stromberg
Spark plugs: 2 B.G. per cylinder 1 XA

The 1928 Dayton Bear was a modified Hall-Scott A-7 engine. Equipment included a hub for a wooden propeller, exhaust flanges. Instruction book, and tool kit.
Accessories available at extra cost were a fuel pump drive, C-5 fuel pump, starter, and hub for a steel propeller.
Type: 4 cylinder inline, air cooled
Approved Type Certificate No.11
Military Rating: 110 hp at 1500 rpm
Rating: 120 hp at 1850 rpm
Displacement: 445 cu.in
Compression ratio: 5.1-1
Bore: 4 1/2 in
Stroke: 7 in
Length: 50 3/32 in
Width: 18 1/4 in
Height: 38 27/32 in
Weight: 375 lb
Fuel consumption: not more than .525 lb/hp/hr
Oil consumption: not more than .0125 lb/hp/hr
Lubrication: Force feed
Ignition: 2 Dual Bosch magnetos
Carburation: Zenith L-8
Spark plugs: 2 per cylinder B.G. 1 XA.
Price: $1450