The Stinson Junior was a high-winged

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monoplane of the late 1920s, built for private owners, and was one of the first such designs to feature a fully enclosed cabin.

Design and development

Stinson Aircraft had introduced their large high-winged six-seat SM-1 Detroiter in 1927. The SM-1 was sold successfully to airlines and other commercial operators, but it was too large to appeal to private owners. Stinson therefore redesigned the aircraft with shorter span wings, shorter fuselage and a choice of less powerful engines as the SM-2 Junior. The aircraft was a strut-braced high-wing monoplane with a sturdy outrigger undercarriage which was braced against the wing support struts and the initial 110 h.p. Warner Scarab engine was normally left uncowled. The first SM-2 flew in mid-1928 and deliveries commenced that year. Later versions of the SM-2 had higher-powered engines of between 165 h.p. and 225 h.p. The design was further developed to produce the more powerful and heavier SM-7 and SM-8 models which were full four-seaters and these were also used by commercial firms. The Junior R of 1932 had a deeper fuselage and a low-set stub wing to mount the undercarriage and wing struts.

Operational history

The various Stinson Junior models were in production between 1928 and 1933, being bought by both wealthy private flyers and commercial enterprises. A total of 321 Juniors were built, of which 27 survived in 2001 and several of these were airworthy in private hands. In 1977, the

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painted an SM-8A "Spirit of EAA", and flew a cross-country tour as the support plane with a "spirit of St. Louis" replica as part of the 50th anniversary of Lindbergh's Trans-Atlantic crossing.

Variants

(per Simpson, 2001, pp. 523–524) ;SM-2 : Warner Scarab 110 h.p. ;SM-2AA :

Wright J6-5 The Wright R-540 Whirlwind was a series of five-cylinder air-cooled radial aircraft engines built by the Wright Aeronautical division of Curtiss-Wright. These engines had a displacement of 540 in³ (8.85 L) and power ratings of around ...

165 h.p. ;SM-2AB :

Wright J5 The Wright R-790 Whirlwind was a series of nine-cylinder air-cooled radial aircraft engines built by Wright Aeronautical Corporation, with a total displacement of about and around . These engines were the earliest members of the Wright Whirlwin ...

220 h.p. ;SM-2AC :

Wright J6-7 The Wright R-760 Whirlwind was a series of seven-cylinder air-cooled radial aircraft engines built by the Wright Aeronautical division of Curtiss-Wright. These engines had a displacement of 756 in³ (12.4 L) and power ratings of 225-350 ...

225 h.p. ;SM-2ACS: floatplane version of the SM-2AC ;SM-7A :

Wright J6-9 The Wright R-975 Whirlwind was a series of nine-cylinder air-cooled radial aircraft engines built by the Wright Aeronautical division of Curtiss-Wright. These engines had a displacement of about and power ratings of . They were the largest membe ...

300 h.p. ;SM-7B : Wasp Junior 300 h.p. ;SM-8A : Lycoming R-680 215 h.p. ;SM-8B : Wright J6-7 225 h.p. ;SM-8D :

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DR-980 diesel 225 h.p. ;Junior R : Lycoming R-680 215 h.p. and deeper fuselage. 28 Units built ;Junior R-2 : Lycomong R-680-BA 240 h.p. 3 Built. ;Junior R-3 : as R-2 with retractable undercarriage 3 Units built. ;Junior R-3-S : Lycoming R-680-6 245 h.p. ;Junior S : Lycoming R-680 215 h.p. with fully cowled engine ;Junior W : generally similar to the SM-7B, powered by a Wasp Junior engine

Specifications (SM-2AC)

References

;Notes ;Bibliography * *

External links

aerofiles

Stinson "S" Junior, NC-10888
{{Stinson aircraft Junior 1920s United States civil utility aircraft High-wing aircraft Single-engined tractor aircraft Aircraft first flown in 1928