The
de Havilland
Canada DHC-3 Otter
is a single-engined, high-wing,
propeller-driven,
STOL aircraft developed by de Havilland
Canada. It was conceived to be capable of
performing the same roles as the earlier and
highly successful
Beaver, but was overall a larger
aircraft. When
de Havilland Canada began design work on the
"King Beaver" (the Otter's original name) in
January 1951, it was trying to extend the
company's line of rugged STOL utility
transports that had begun with the Beaver.
The single-engined, high-wing,
propeller-driven DHC-3 Otter was conceived
to be capable of performing the same roles
as the Beaver, but was considerably larger,
the veritable "one-ton truck" (in company
parlance, the Beaver was the "half-ton
truck").
Using the same
overall configuration of the earlier and
highly successful DHC2 Beaver, the new
design incorporated a longer fuselage,
greater-span wings, a cruciform tail, and
was much heavier. Seating in the main cabin
is for 10 or 11, whereas the Beaver could
seat six. Power is supplied by a 450-kW (600
hp) Pratt & Whitney Wasp radial. Like the
Beaver, the Otter can be fitted with skis or
floats. The Otter served as the basis for
the very successful Twin Otter, which
featured two wing-mounted Pratt & Whitney
Canada PT6 turboprops.
The Otter received
Canadian certification in November 1952 and
entered production shortly thereafter.
Modifications
Stolairus
Aviation of Kelowna, BC has developed
several modifications for the DHC-3
including a STOL Kit, which modifies the
wing with a contoured leading edge and
drooped wingtips for increased performance.
Stolairus has also developed a 400 lb
"upgross" kit which increases the gross
weight of the DHC-3 to 8,367 lbs on floats.
Some aircraft were
converted to turbine power using a PT6A,
Walter 601 (manufactured in the Czech
Republic), or Garrett/Honeywell TPE331-10,
by Texas Turbine Conversions. The Walter
M601E-11 Turbine Engine conversion is
manufactured and installed by Stolairus
Aviation.
A Polish
Pezetel radial engine has also been fitted.
Re-engined aircraft have been offered since
the 1980s by Airtech Canada as the
DHC-3/1000
using current-production 1,000 hp (745 kW)
PZL ASz-62 IR radials.
Variants
- DHC-3
Otter :
Single-engined STOL utility transport
aircraft.
-
CSR-123 Otter
: STOL utility transport aircraft
for the Royal Canadian Air Force.
- YU-1
Otter
: Six test and evaluation aircraft
for the U.S. Army.
- U-1A
Otter
: STOL utility transport aircraft
for the US Army.
- UC-1
Otter
: STOL utility transport aircraft
for the United States Navy. Later
redesignated
U-1B Otter
in 1962.
- DHC-3-T
Turbo-Otter
: Otter fitted with either a PT6A-27 or
PT6A-34 turboprop engine.
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SPECIFICATIONS:
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PERFORMANCE: |
Span:
58 ft 0 in (17.69 m) |
Maximum speed:
160 mph (139 knots, 257 km/h) |
Length:
41 ft 10 in (12.80 m) |
Cruising speed:
121 mph (105 knots, 195 km/h) at sea
level (econ cruise) |
Height:
12 ft 7 in (3.83 m) |
Range:
945 mi (822 nmi, 1,520 km) |
Empty Weight:
4,431 lb (2,010 kg) |
Service ceiling:
18,800 ft (5,730 m) |
Gross Weight:
8,000 lb (3,629 kg) |
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Crew:
Pilot and up to 10 passengers |
Engines:
1 × Pratt & Whitney R-1340-S1H1-G Wasp
9-cylinder air-cooled radial engine, 600
hp (448 kW) |
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SOURCE:
Wikipedia |
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