From Wikipedia, the free encyclopedia
SM-6000 Airliner
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Stinson SM-6000B Airliner trimotor circa 1965 when owned by RP Rice of Kennett, MO.
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Role
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Three-engined airliner
Type of aircraft
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National origin
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United States
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Manufacturer
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Stinson Aircraft Corporation
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Number built
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53 (SM-6000)
24 (Model U)
[1]
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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-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
]
- ^
Wegg 1990, p.118.
- ^
Donald M. Pattillo.
A History in the Making: 80 Turbulent Years in the American General Aviation Industry
. p. 10.
- ^
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.
- ^
a
b
c
d
e
f
Gradidge 1989, p. 18
- ^
"Stinson Trimotors - Holcomb's Aerodrome"
.
- ^
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
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Model numbers
| Detroiter
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Junior
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Reliant
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Airliner
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Vultee
models
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Convair
models
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One off designs
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Names
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Military
designations
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Army/Air Force sequence
(1925-1962)
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Tri-service sequence
(1962-present)
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Revived original sequence
(2005-present)
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Non-sequential designations
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Related designations
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1
Not assigned •
2
Assigned to multiple types •
3
Unconfirmed
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