A 30 horsepower 4-cylinder engine also built under licence by Bariquand & Marré of Paris in 1909.
Engines – Power
Wright L

The 1915 Wright L was a two-place, open cockpit biplane primary trainer with standard control surfaces. Powered by a 100hp Hall-Scott A-7, it was similar to the Dayton-Wright FS-1 except for a longer wing.

The Model L was inferior to many other biplanes that were being produced at the time. It failed to secure any military orders and few were produced.
This was the last airplane produced by the Wright Company under that name. By this time Orville Wright no longer owned the company, but he was retained as a consultant and may have had some input on the design of the Model L.

Wright Model L
Engine: 100hp Hall-Scott A-7, 75 hp at 1400 to 1560 rpm
Propeller: Single direct-drive, 8 ft (244 cm)
Wingspan: 29 ft (8.8 m)
Wing area: 360 sq ft (33.4 sq. m)
Wing chord: 6.5 ft (198 cm)
Wing separation: 5.7 ft (174 cm)
Camber: 1:20
Length: 24.2 ft (7.4 m)
Horizontal rear elevator: 20 sq ft (1.9 sq m)
Twin movable vertical rear rudders: 8.5 sq ft (0.8 sq m)
Weight: 850 lbs (386 kg)
Speed range: 25 to 80 mph (40 to 129 kph)

Wright K

The Wright K of 1916 featured chain-driven, interwing-mounted twin props, powered by a 60-70hp Wright engine. One was built, going to the USN as AH-23 / A51.
Wright J / Long Bull
The 1915 Wright J, or Long Bull (Burgess), was a two-place, open-cockpit, biplane floatplane similar to the Aeroboat. It was a license-built civil version of the Burgess-Wright C.
Wright I / Coastal Defense Hydro
The 1914 Wright I, also seen as Coastal Defense Hydro, was a two-place, open-cockpit, biplane floatplane for the Signal Corps as SC17.
Wright F3W Apache / XF3W Apache

After the U.S. Navy declared its preference for radial engines, Wright developed the P-1 Simoon. To demonstrate the engine, the F3W was designed to carry it. The new air-cooled, supercharged 1,176.036-cubic-inch-displacement (19.272 liters) Wright Aeronautical Division R-1200 Simoon 9-cylinder radial engine, was rated at 350 horsepower at 1,900 r.p.m. The R-1200 weighed 640 pounds (290 kilograms). The F3W was a single-seat biplane, with a steel tubing fuselage and wood wings, covered by fabric. Designed to be a carrier-based fighter and powered by the Simoon engine, its performance was poor. One was built, A7223, and tested XF3W-1. After the Navy took delivery of the aircraft, they installed a rival company’s engine, the number two Pratt & Whitney R-1340 radial Wasp A engine. The aircraft was redesignated XF3W, and flew with the new engine for the first time on 5 May 1926. The XF3W-1 was the first airplane to fly with a Pratt & Whitney Wasp engine.
The Navy used the XF3W as a test bed for the Pratt & Whitney engine until 1930, during which time the aircraft set a number of records.
On 6 September 1926, the XF3W set the world altitude record for seaplanes of 38,500 ft (11,700 m). On 8 May 1929: Lieutenant Apollo Soucek, United States Navy, set a Fédération Aéronautique Internationale (FAI) World Record for Altitude when he flew the prototype Wright Aeronautical Division XF3W-1 Apache, Bu. No. A7223, to 11,930 meters (39,140 feet) over NAS Anacostia, Washington, D.C. The record was certified by the National Aeronautic Association. Lieutenant Soucek was awarded the Distinguished Flying Cross for this achievement.

The National Advisory Committee for Aeronautics (NACA) used the XF3W-1 for engine and cowling tests at the Langley Memorial Aeronautical Laboratory (LMAL), Langley Field, Hampton, Virginia. Which engine was installed at the time of Lieutenant Soucek’s record flight is uncertain.

The XF3W-1’s engine was supercharged by a NACA Model 2E Roots-type supercharger, built by the Allison Engineering Company. This supercharger, serial number 1, is in the collection of the National Air and Space Museum.
Lieutenant Soucek set two other World Records with the XF3W-1 Apache. On 4 June 1929, with the Apache configured as a float plane, he flew it to an altitude of 11,753 meters (38,560 feet). The following year, 4 June 1930, he flew the Apache to 13,157 meters (43,166 feet). The XF3W was fitted with a single centreline float to evaluate the concept of basing floatplanes on battleships.
XF3W-1 with floats
Engine: 1 × Pratt & Whitney R-1340-B, 450 hp (336 kW)
Wingspan: 27 ft 4 in (8.33 m)
Wing area: 215 sq.ft (19.97 sq.m)
Length: 22 ft 1 in (6.73 m)
Height: 8 ft 6 in (2.59 m)
Empty weight: 1,414 lb (641 kg)
Gross weight: 2,128 lb (965 kg)
Maximum speed: 162 mph (261 km/h)
Service ceiling: 38,560 ft (11,753 m)
Crew: 1
Wright F2W

Two Wright F2W-1 were built for the US Navy in 1923 as Pulitzer racers A6743 and A6744. First flying on 27 August 1923, piloted by L H Sanderson, the first crashed on landing during trials and was damaged beyond economical repair.
A6744 was converted to twin floats as F2W-2 in 1924, but also crashed during testing.

Engine: Wright T-3 Tornado, 780hp
Wingspan: 22’6″
Length: 21’4″
Speed: 248 mph
Ceiling: 36,300′
Seats: 1
Wright D Scout / Army scout
The Wright D Scout, or Army scout, of 1913 were single place, open cockpit biplanes. Two were built for the Signal Corps as SC19 and SC20.
Engine: Wright 6-60, 50hp
Wingspan: 26′ 6″
Length: 24’11”
Speed: 67 mph
Seats: 1
Wright H / HS

The 1914 Wright H featured twin chain-driven propellers and a boat-like fuselage. Five long- and short-nosed versions were produced.

The Wright HS was a 1915 version with shorter-span wings than its Model F predecessor and saw service in the Mexican border campaign.

Engine: Wright, 60hp
Wingspan: 32’0″
Length: 26’6″
Speed: 100 mph
Seats: 2
Wright F / Tin Cow / Burgess-Wright F

The 1913 Wright F, or Tin Cow, was the first of the fuselage models, but it still retained wing-warping and two chain-driven propellers.

Although this designation is often seen applied to the Model B built under license by Burgess as their model F, only one was ever produced by the Wrights, delivered in 1914 to US Signal Corps as SC39.

W.Burgess built the Burgess-Wright F in 1911.

The Model F evolved into the 1915 model HS.
Engine: Austro-Daimler 6, 90 hp
Wingspan: 42’0″
Length: 29’6″
Speed: 60 mph
Seats: 2
Burgess-Wright F
Span: 39’2″
Length: 29’6″
Seats: 2