Spartan C2

Spartan C2-60 NC11902

By 1931 Spartan was producing low-wing side-by-side 2-seaters, further developed as C2-60. Designed by Willis Brown and selling for $2,245, the prototype NC11000 was under ATC 2-370.

Sixteen C2-60 were built ATC 427; NC11000, NC11015 and NC11016, NC11021 to 11023, and NC11900 to NC11909.

Two, NC992N and NC993N (ATC 2-408), were built as C2-165 instrument trainers with 165hp Wright J-5 engines and hooded cockpits for the Spartan School of Aeronautics.

C2-60
Engine: 55hp Jacobs L-3
Wingspan: 40’0″
Length: 22’5″
Useful load: 464 lb
Max speed: 93 mph
Cruise: 81 mph
Stall: 39 mph
Range: 320 mi
Ceiling: 13,000 ft
Seats: 2

C2-165
Engine: 165hp Wright J-5
Seats: 2

Spartan C3

First flying on 25 October 1936, the three-seat, open cockpit Spartan C3 was built with various engines.

Spartan C3 Pretty (ad: Aero Digest)

Designed by Willis Brown, the 1928 125hp Ryan-Siemens powered C3-1 (ATC 71) was priced at $5,200. About 100 were built.

Spartan C3-1 NX1208

Four of the 1928 C3-2 (ATC 73) were built (N8063, NC10003, NC10080, NC11985) powered by a 120hp Walter, redesignated C3-120 in 1929

Spartan C3-120 N8063

The 1929 thee-seat C3-3 (ATC 2-77) was powered by a 170hp Curtiss Challenger engine.

The 1929 C3-4 (ATC 2-78) was powered by a 115hp Axelson A engine.

The 1929 C3-5 (ATC 2-79), later re-designated C3-165, was powered by a 165hp Wright J-5 engine.

Spartan C3-165 Brochure art – NC8070

Over forty of the 1929 C3-165 (ATC 195) were built, priced at $6,750 and increasing to $5,975 in 1930.

Only one C3-166 (ATC 290) was built, NC707N. Built in 1929 it was similar to the C3-165, powered by a 165hp Comet 7-E engine, and priced at $5,675.

C-3-225

Fourteen of the 1930 C3-225 (ATC 286) were built, powered by a 225hp Wright J-6 engine, and priced at $7,750.

Spartan C3-225 Brochure art

C3-1
Engine: 125hp Ryan-Siemens
Wingspan: 32’0″
Length: 23’6″
Useful load: 800 lb
Max speed: 115 mph
Cruise: 98 mph
Stall: 42 mph
Range: 450-500 mi
Ceiling: 11,000 ft

C3-2 / C3-120
Engine: 120hp Walter

C3-3
Engine: 170hp Curtiss Challenger
Seats: 3

C3-4
Engine: 115hp Axelson A

C3-5 / C3-165
Engine: 165hp Wright J-5

C3-165
Engine: 165hp Wright J-6
Length: 23’2″
Useful load: 905 lb
Max speed: 115 mph
Cruise: 100 mph
Stall: 45 mph
Range: 500+ mi

C3-166
Engine: 165hp Comet 7-E

C3-225
Engine: 225hp Wright J-6;
Length: 23’3″
Useful load: 959 lb
Max speed: 130 mph
Cruise: 110 mph
Stall: 55 mph
Range: 460 mi

Spartan G-3

Early in 1927 Spartan G-3 three-seat open-cockpit biplane was built by Mid-Continent Aircraft Company.

Designed by Willis Brown, the prototype first had a 100hp LeRhône rotary, later changed to a 125hp Ryan-Siemens.

Engine: 125hp Ryan-Siemens
Wingspan: 32’0″
Length: 23’6″
Useful load: 800 lb
Max speed: 115 mph
Cruse: 93 mph
Stall: 37 mph
Range: 600 mph
Seats: 3

Spartan Aircraft Co

1927: Mid-Continent Aircraft Co, Tulsa OK.
Early in 1927 Spartan G-3 three-seat open-cockpit biplane was built by Mid-Continent Aircraft Company.

Mid-Continent was reorganized as Spartan Aircraft Co in 1928 at Tulsa, Oklahoma.

Built C-3 with Ryan-Siemens engine. Continued to build biplanes but by 1931 was producing series of 4/5-seat cabin monoplanes; also low-wing side-by-side 2-seaters, further developed as C2-60. Spartan Executive 4/5-seat all-metal monoplane of 1936 converted in 1938 to Zeus 2-seat military type; a few of which supplied to China and Mexico. In 1940 U.S. Navy ordered 201 Spartan NP-1 biplane trainers for new Naval Reserve schools.

In 1945 production switched from airplanes to house trailers.

1968: Spartan interests sold to Automation Industries Inc.

1972: Company purchased by National Systems Corp.

1994: Spartan School still active.

Spainhour 1912 monoplane

The monoplane of James S. Spainhour, of Pittsburgh, PA, had an unusual device for securing lateral control. The wings did not warp, or only very slightly. They were fixed to the fuselage by a floating bridge, and the angle of incidence of the whole of each wing could be altered by the movement of a pedal, one for each plane. When the angle of incidence of both the wings is increased the machine pitched up. The machine weighed 497 pounds, had a triangular fuselage and a span of 34 feet 5 inches. It was powered by a 40 hp four-cylinder Kowalsky engine, which had a self-starting crank. Spainhour made several short flights near Pittsburgh on a six-acre field, and moved to Mineola, Long Island, to get more room.

It apparently reached 1000′ high at speed of 50 mph

SPAD S.54

The SPAD S.54 was a French biplane trainer aircraft of the early 1920s, developed by Société Pour L’Aviation et ses Dérivés (SPAD).

Designed by Louis Béchéreau, the S.54 first flew on 23 February 1922.

Twenty-five were built, operated by the Aéronautique Militaire.

Engine: 1 × Clerget 9B, 97 kW (130 hp)
Wingspan: 8.96 m (29 ft 5 in)
Wing area: 23.52 m2 (253.2 sq ft)
Length: 7.24 m (23 ft 9 in)
Height: 2.57 m (8 ft 5 in)
Empty weight: 520 kg (1,146 lb)
Gross weight: 757 kg (1,669 lb)
Maximum speed: 120 km/h (75 mph, 65 kn)
Crew: 2