Stinson Airliner

From Wikipedia, the free encyclopedia
SM-6000 Airliner
Stinson SM-6000B Airliner trimotor circa 1965 when owned by RP Rice of Kennett, MO.
Role Three-engined airliner
National origin United States
Manufacturer Stinson Aircraft Corporation
Number built 53 (SM-6000)
24 (Model U) [1]

The Stinson SM-6000 Airliner was a 1930s three-engined ( trimotor ) ten-passenger airliner designed and built by the Stinson Aircraft Corporation . The SM-6000 was a high-wing braced monoplane with room for a pilot and a cabin for ten passengers. It was powered by three 215 hp (160 kW) Lycoming R-680 engines strut-mounted one each side above the main landing gear units and one in the nose. A number of variants were built mainly with improved interiors. In 1932 the Model U Airliner was produced which had low-set stub wings with an engine mounted at each wingtip.

Variants [ edit ]

Corman 6000
The initial prototypes produced by the Corman aircraft Co. as part of the E L Cord empire. [2]
SM-6000 Airliner
1930 initial production variant with three 215hp (160kW) Lycoming R-680 engines.
SM-6000-A Airliner
1930 variant available with different interior configurations.
SM-6000-B
SM-6000-B1 Airliner
1931 all-passenger variant with better interior equipment.
SM-6000-B2 Airliner
As the B1 but with a mixed mail/passenger interior.
Model U Airliner
1932 improved model with three 240hp (179kW) Lycoming R-680-BA engines on stub wings.
C-91
United States military designation for one SM-6000-A (s/n 42-79547) impressed into service in 1942.

Survivors [ edit ]

Only two of these high-wing models are known to exist. One is owned and operated by Mid America Flight Museum in Mount Pleasant, TX , the other by Kermit Weeks and is maintained in airworthy condition at Fantasy of Flight in Polk City, Florida .

[3]

Operators [ edit ]

  United States
  Philippines

Specifications (SM-6000-B) [ edit ]

Data from [5] [6]

General characteristics

  • Crew: two
  • Capacity: ten (B1), eight (B2)
  • Length: 42 ft 0 in (12.8 m)
  • Wingspan: 60 ft 0 in (18.29 m)
  • Height: 12 ft 0 in (3.66 m)
  • Wing area: 490 sq ft (45.6 m 2 )
  • Empty weight: 5,670 lb (2,620 kg)
  • Gross weight: 8,600 lb (3,910 kg)
  • Powerplant: 3 × Lycoming R-680 , 215 hp (160 kW) each

Performance

  • Maximum speed: 146 mph (234 km/h, 127 kn)
  • Cruise speed: 125 mph (200 km/h, 109 kn)
  • Range: 390 mi (628 km, 340 nmi)
  • Service ceiling: 14,200 ft (4,330 m)
  • Rate of climb: 1,000 ft/min (5.1 m/s)

Notes [ edit ]

  1. ^ Wegg 1990, p.118.
  2. ^ Donald M. Pattillo. A History in the Making: 80 Turbulent Years in the American General Aviation Industry . p. 10.
  3. ^ As pictured on timetable, March 21, 1934, Boston Maine Airways Central Vermont Airways, and other schedules; pictured in Boston and Maine Airways employee magazine, "Boston-Maine Airways, Inc., Take Air Again in Year-Round Service;" circa 1933; discussed at length by Robert W. Mudge in Adventures of a Yellowbird: the biography of an airline, Branden Press, 1969.
  4. ^ a b c d e f Gradidge 1989, p. 18
  5. ^ "Stinson Trimotors - Holcomb's Aerodrome" .
  6. ^ Wegg 1990, p.128.

References [ edit ]

  • Gradidge, J. M. G. (November 1989). "American Classics: Stinson SM-6000". FlyPast . No. 100. p. 18. ISSN   0262-6950 .
  • Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation . London: Studio Editions.
  • Wegg, John (1990). General Dynamics Aircraft and their Predecessors . London: Putnam Aeronautical Books. ISBN   0-85177-833-X .
  • The Illustrated Encyclopedia of Aircraft (Part Work 1982-1985) . Orbis Publishing.

External links [ edit ]

Media related to Stinson SM-6000 at Wikimedia Commons