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  2. Standard J - Wikipedia

    en.wikipedia.org/wiki/Standard_J

    The Standard J is a two-seat basic trainer two-bay biplane produced in the United States from 1916 to 1918, powered by a four-cylinder inline Hall-Scott A-7a engine. It was constructed from wood with wire bracing and fabric covering.

  3. Aerial Engineering Corporation Standard 6W-3 - Wikipedia

    en.wikipedia.org/wiki/Aerial_Engineering...

    The Aerial Engineering Corporation Standard 6W-3 was a commercial transport modification of the US Standard J-1 biplane military trainer aircraft, with new wings, engine and accommodation for four passengers. First flown in 1925, it was built in small numbers.

  4. Curtiss JN Jenny - Wikipedia

    en.wikipedia.org/wiki/Curtiss_JN_Jenny

    Curtiss Stinson Special (1918) — a custom-built, single-seat aircraft for Katherine Stinson, constructed from the fuselage of a Curtiss Model S plus new biplane wings and JN-4 tail surfaces, powered by a 100-hp (74.5-kW) OXX-6 [32]: 136 [33] [f]

  5. Standard Aircraft Corporation - Wikipedia

    en.wikipedia.org/wiki/Standard_Aircraft_Corporation

    The corporation supplied the Sloane H as the Standard H-2 and H-3 to the Army, and the float-equipped H-4H to the Navy, after the Sloane company was reorganised as the Standard Aircraft Co. A more significant type was the Standard J series trainer , similar to the Curtiss JN-4 , which began with the SJ prototype, followed by the production J-1 ...

  6. Lincoln Standard L.S.5 - Wikipedia

    en.wikipedia.org/wiki/Lincoln_Standard_L.S.5

    The L.S.5 was a modification to the Standard J Biplane. The aircraft featured an engine upgrade to 150 hp (112 kW) from the original Curtiss OX-5 engine and a modification to the fuselage to seat four passengers in an unusually deep open cockpit layout with side-by-side configuration seating facing each other. [4]

  7. EAA Biplane - Wikipedia

    en.wikipedia.org/wiki/EAA_Biplane

    Data from Jane's All The World's Aircraft 1965–66. General characteristics Crew: 1 Length: 17 ft 0 in (5.18 m) Wingspan: 20 ft 0 in (6.10 m) Height: 6 ft 0 in (1.83 m) Wing area: 108 sq ft (10.0 m 2) Empty weight: 710 lb (322 kg) Gross weight: 1,150 lb (522 kg) Fuel capacity: 18 US gal (15 imp gal; 68 L) Powerplant: 1 × Continental C85 air-cooled flat-four engine, 85 hp (63 kW) Performance ...

  8. Curtiss JN-6H - Wikipedia

    en.wikipedia.org/wiki/Curtiss_JN-6H

    Developed from the one-off JN-5H advanced trainer, the 6H had a superior aileron operation mechanism. It was used in a variety of roles, with stick and rudder in either one seat or both: JN-6HB single-control bomber trainer (154 built), JN-6HG-1 dual-control gunnery trainer (560 built), JN-6HG-2 single-control gunnery trainer (90 built), JN-6HO single-control observation trainer (106 built ...

  9. Culp Special - Wikipedia

    en.wikipedia.org/wiki/Culp_Special

    The aircraft is made from welded steel tubing and wood, all covered in doped aircraft fabric. Its 24.00 ft (7.3 m) span wing has a wing area of 161 sq ft (15.0 m 2 ). The standard engine used is the Russian 360 hp (268 kW) Vedeneyev M14P nine cylinder, air-cooled, four stroke radial engine .