De Havilland Canada DHC-2 Beaver

· Airtech Canada

Airplanes

Length

9.144 m

Flat Wing Span

14.6304 m

Height

2.7432 m

Flat Wing Area

23.2258 m²

Max Seating

Cruise Speed

230.1362 km/h

Max Speed

255 km/h

Max Ceiling

5486.4 m

Number of Engines

First Flight

1947-08-16

Entry Into service

1948-01-01

Number Built

1657

Total Fuel Capacity

359.1411

Maximum Range

732.2515 km

Pictures

No pictures yet for this family.

Aircraft	Total Fuel Capacity	Maximum Range (km)
De Havilland Canada DHC-2 Beaver	359.1411	732.2515

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)
BFW N.I	Mercedes D.IVa	9.2	14.5	Compare
Comte AC-8		9.2	14.5	Compare
Albatros C.X	Mercedes D.IVa	9.15	14.36	Compare
Aeromarine 39		9.144	14.3256	Compare
Caproni Ca.53		9.23	14.3	Compare
Bristol Seely	Siddeley Puma	8.99	14.4	Compare

All data (26 fields)

Name: De Havilland Canada DHC-2 Beaver
Manufacturer: Airtech Canada
Description: The de Havilland Canada DHC-2 Beaver is a single-engined high-wing propeller-driven short takeoff and landing (STOL) aircraft developed and manufactured by de Havilland Canada.
First Flight: 1947-08-16
Entry Into service: 1948-01-01
Production End: 1967-01-01
Designer: Airtech Canada
Type: STOL utility transport
Length (m): 9.144
Height (m): 2.7432
Cockpit Crew: 1
Max Seating: 6
Max Speed (km/h): 255
Cruise Speed (km/h): 230.1362
Max Ceiling (m): 5486.4
Rate of Climb (m/s): 5.1816
Capacity Description: 6 passengers, 2,100 lb (953 kg) useful load
National Origin: Canada
Number Built: 1657
Powerplant Description: 1 × Pratt & Whitney R-985 Wasp Jr. 9 cylinder radial engine, 336 kW (450 hp) each
Primary Users: regional and remote air carriers, United States Army, Civil Air Patrol
Status: In service
Wikipedia Article (URL): en.wikipedia.org/wiki/De_Havilland_Canada_DHC-2_Beaver
Flat Wing Span (m): 14.6304
Flat Wing Area (m²): 23.2258
Number of Engines: 1