In 1918 Eino Salminen built a monoplane.
1 engine
Salisbury biplane
In 1927 H M Salisbury of Walnut Grove CA built a single place open cockpit biplane ultralight.
Engine: 15hp Pope motorcycle
Wingspan: 20’0″
Length: 13’0″
Saint-Hubert 135 B.O.

A Belgian touring plane, the Saint-Hubert 135 B.O. low-wing monoplane, constructed by the Saint-Hubert Aircraft Engineering Works and designed by Mr. Pierre Baudoux (of Brussels University) and Mr. J. Orta, of the Saint-Hubert Aerodrome. It is equipped with a “Cirrus-Hermes IV” engine, and has a maximum speed of 152 mph and a cruising speed of 127 mph.
Salina-Hoffman Susie Bee
Over a period of six years, Louis E Salina & Earl Hoffman built a single place open cockpit biplane for $2,000. Registered N1116U, the single model built first flew on 2 Jul 1967.
Engine: Lycoming O-290-G
Wingspan: 15’5″
Length: 15’2″
Max speed: 170 mph
Cruise speed: 145 mph
Stall: 65 mph
Range: 450 mi
Saito 1912 Aeroplane

Sotoichi Saito of Tsuruoka City, Yamagata Prefecture, had been involved in the development of balloon flight since 1889. In 1910 he bought a 50hp Gnome engine from France so that he could study aero-engines. He later acquired a patent for a ‘Flying Machine’ and manufactured an aircraft resembling a Bleriot monoplane. Helping with this project was Shotaro Ueda. Single-engine monoplane. Wooden structure with fabric-covered wing and uncovered fuselage structure.
The aeroplane contained some rather innovative features. For protection against inflight fire, the fuel tank was installed on struts high above the rear fuselage at a considerable distance from the engine. Another feature was that in the event of an inflight emergency, a cable could be pulled, causing the fuselage and engine to separate from the wings leaving the pilot still seated on the wing section which was to act as a parachute.
Saito named his aeroplane the Saigai, an acronym derived from his own name. In june 1912 he tested the aeroplane on the dry bed of the Akagawa River in Tsuruoka City. The aeroplane, piloted by Suketaro Koya, was put on a special railway track for take off. Koya was probably selected because of his engine experience in operating the Mogami Maru river boat. Soon after becoming airborne, Koya felt that further flight would be risky and pulled the emergency cord, thus destroying the aeroplane. The Gnome engine was salvaged and installed in the Tamai 3 Aeroplane in 1917, in which the pilot, Seitaro Tamai, was killed. The engine then passed to Shigesaburo Torigai, and still later was installed in the Tsurubane No.2 Aeroplane of Otojiro Itoh, which made the first loop by a Japanese civil aeroplane when piloted by Toyotaro Yamagata in 1918.
Engine: 50hp Gnome
Propeller: two-blade wood
Span: 10.30m (33ft 9 1/2in)
Length: 9.10m (29ft 10 1/4in)
Loaded weight: 560kg (1,234Ib)
SAIMAN 202-M / 204

The Italian Saiman 202-M was first introduced in 1936 and participated in a number of international competitions in pre-war years. During the war the type was employed as a liaison and communications two-seat cabin monoplane by the Regia Aeronautica.
Construction is all-wood with fabric and plywood covering. The Saiman 202-M is powered by a 130 hp Alfa Romeo 110 engine.
The Saiman 204 is generally similar but is arranged as a four-seater and has a 180 hp Alfa Romeo 115 engine.
Saiman 202-M
Engine: 130 hp Alfa Romeo 110
Wing span: 35 ft 7 in
Wing area: 190 sq.ft
Length: 25 ft 3 in
Height: 6 ft 7 in
Empty weight: 1364 lb
Loaded weight: 2068 lb
Max speed: 143 mph
Cruise: 124 mph
Absolute ceiling: 16,400 ft
Range: 683 mi
Seats: 2
Saiman 204
Engine: 180 hp Alfa Romeo 115
Seats: 4
Sagstetter monoplane
In 1935 Clarence & Raymond Sagstetter built two single place open cockpit monoplanes. The were registered N14813 c/n 15207 to Raymond Sagstetter and N14814 c/n 12570 to Clarence Sagstetter. U
Ultralights with identical specifications, the engines were Sagstetter home-built (or modified) 30hp Sagstetter engines.
Safe-Wings SW-1 / SW-2
The 1937 SW-1 was a two place cabin monoplane was registered NX18220, and powered by a 40hp Continental A-40 engine. The one built was modified, as the SW-2, with a 60hp Milwaukee Tank engine.
SAETA JN-01

Sadler A-22 Lasa
A 1989 light-armed, twin-boom surveillance aircraft. A single place enclosed midwing monoplane with retractable undercarriage, one built, first flying on 10/8/89, registered N22AB.
Engine: 300hp Chevrolet V-6 pusher
Wingspan: 22’0″
Length: 15’8″
Useful load: 1300 lb
Max speed: 190 mph
Stall speed: 72 mph
Range: 300 mi