De Havilland Canada DHC-2 Beaver

Summary

Category Other aircraft
Origin country 🇨🇦 Canada
First flight16 August 1947
Year of introduction1948
Number produced1657 units

Description

The De Havilland Canada DHC-2 Beaver is a military aircraft that was developed in Canada during the 1940s. It was primarily designed as a utility transport and reconnaissance aircraft. The DHC-2 Beaver has a rugged design and a high-wing configuration, allowing it to operate in challenging terrain and adverse weather conditions. It has been deployed for various missions, including cargo transportation, aerial surveying, and search and rescue operations. The aircraft's versatility and durability have made it popular among military forces around the world. Its ability to operate on unprepared runways and its capability to carry significant payloads have made it an asset in remote and austere environments.

Technical specifications

Version: DHC-2 Beaver I
Crew1 pilot
Maximum speed 254 km/h (158 mph)
Wing area23 m² (247.6 sqft)
Wingspan15 m (49.2 ft)
Height2.7 m (9.0 ft)
Length9.2 m (30.3 ft)
Service ceiling5486 m (17999 ft)
Empty weight1361 kg (3000 lbs)
Climb rate5.2 m/s (17.1 ft/s)
Powerplant1 × pistons engine Pratt & Whitney R-985-AN-1 delivering 336 kW

Current operating countries

Country Units
United States United States 2

Numbers in parentheses, e.g. '(+5)', indicate units ordered but not yet delivered.

All operators

ArgentinaAustraliaAustriaChileColombiaCubaDominican RepublicFinlandUnited KingdomGhanaGreeceIndonesiaIranCambodiaNetherlandsNew ZealandPanamaPeruPhilippinesParaguayThailandTurkeyUnited StatesYemen • Ex-Yugoslavia • Zambia

Photo of DHC-2 Beaver

Photo of DHC-2 Beaver Credits: Jeroen Stroes Aviation Photography