De Havilland Canada DHC-6 Twin Otter
Picture has been licensed under a GFDL license.
Original source: http://www.airliners.net/photo/WinAir/De-Havilland-Canada/2035397/L/
Author: Timo Breidenstein

The DHC-6 Twin Otter is a Canadian 19-passenger STOL (Short Takeoff and Landing) utility aircraft developed by de Havilland Canada and currently produced by Viking Air. The aircraft's fixed tricycle undercarriage STOL abilities and high rate of climb have made it a successful cargo regional passenger airliner and MEDEVAC aircraft. In addition the Twin Otter has been popular with commercial skydiving operations and it is used by the United States Army Parachute Team.

De Havilland Canada DHC-6 Twin Otter - Click here for a bigger picture and more information Photographer: Tom Hildreth Location: Hyannis - Barnstable Municipal 1
DE HAVILLAND CANADA DHC-6 Twin Otter 1DE HAVILLAND CANADA DHC-6 Twin Otter 2DE HAVILLAND CANADA DHC-6 Twin Otter 3DE HAVILLAND CANADA DHC-6 Twin Otter 4 Registration: Year of construction:1977 Total 2
De Havilland Canada DHC-6 Twin Otter equipado con flotadores.3
de Havilland Canada DHC-6 Twin Otter Twin Otter fra British Airways. Bemærk de højt monterede vinger, der også gør flytypen meget anvendelig som udsigtsfly til rundtursflyvning med turister.4

Made by De Havilland CanadaViking AirViking Air -Victoria BCde Havilland CanadaToronto ON.

It is the successor of the De Havilland Canada DHC-3 Otter .

he De Havilland Canada DHC-6 Twin Otter is one of the most versitile aircraft ever designed.5
SKU: CD - DHC-6 The De Havilland Canada DHC-6 Twin Otter is one of the most versatile aircraft ever designed.6
The De Havilland Canada DHC-6 Twin Otter (aka Twotter) is one of those aircraft that should have been replaced by some new aircraft at least a decade ago. But it's not.7
de Havilland Canada DHC-6 Twin Otter in Aviation Safety Network. http://aviation-safety.net/. URL consultato il 01-03-2009. 2.8
Height Main
594.36
601.98
Developed Into
De Havilland Canada Dash 7
Predecessor
De Havilland Canada DHC-3 Otter
Stall Speed Main
58
Length Alt
15.77 m
Max Takeoff Weight Main
12500.0
Jet Or Prop
prop
Range Main
920
Loaded Weight Main
12500.0
Height Alt
5.9 m
5.93 m
Type Of Prop
turboprop engines
Introduced
1966
Max Speed Main
170
Power/mass Main
36288.0
Developed From
De Havilland Canada DHC-3 Otter
Power/mass Alt
6
Capacity
19
22
Cruise Speed Main
150
Max Takeoff Weight Alt
5670.0
Ceiling Main
25000.0
Number Built
846
Crew
Minimum one pilot
commonly two pilots are used in commercial operations. A flight Attendant must be onboard if there are more than 19 passenger seats.
commonly two pilots
A flight attendant must be on board if there are more than 19 passenger seats.
Never Exceed Speed Main
170
Unit Cost
2000000.0
$2
000
000 USD
Loaded Weight Alt
5670.0
Area Main
420.0
Useful Load Alt
2360.0
Span Alt
19.8 m
Plane Or Copter?
Avionics
Federated system
primarily Collins
Honeywell Primus Apex
Power Alt
460
Engine(prop)
Pratt & Whitney Canada PT6
Manufacturer
Number Of Props
2
First Flight
1965-05-20
Production End Year
1965
Wing Loading Main
30
Climb Rate Main
1600.0
Power Main
2448000.0
2700000.0
Production Start Year
1965
Climb Rate Alt
8.1 m-s
Length Main
1577.34
Span Main
65.0
Area Alt
39 m²
Similar Aircraft
* Antonov An-2* Antonov An-28* Antonov An-38* Beechcraft 1900* Britten-Norman Islander* Britten-Norman Trislander* Dornier Do 228* Embraer EMB 110 Bandeirante* Fairchild Swearingen Metroliner* Fairchild Dornier 228* GAF Nomad* British Aerospace Jetstream 31* Harbin Y-12* IAI Arava* LET L-410* Shorts SC.7 Skyvan
Useful Load Main
5200.0
Related
* de Havilland Canada DHC-3 Otter* de Havilland Canada Dash 7
Empty Weight Main
between and 7
500 lb
between and 8
000 lb
Ceiling Alt
7
620 m
Category
Produced
1965
2008
Empty Weight Alt
3400.0
3628.0
Loading Alt
146

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