De Havilland Canada DHC-2 Mk3 Turbo Beaver

Fixed Wing Single Engine

Picture of De Havilland Canada DHC-2 Mk3 Turbo Beaver

Aircraft Information

ICAO Code
DH2T
Manufacturer
De Havilland Canada
Model
DHC-2 Mk3 Turbo Beaver
Aircraft Type
Fixed Wing Single Engine
Primary Role
General Aviation

Technical Data

Engine Type
Turboprop
Engine Model
PT6A-6 or PT6A-20
Production Years
1968-1967
Units Produced
60
First Flight
1947-08-16
Notable Operators
Ontario Department of Lands and Forests, Canadian bush operators, Kenmore Air

The DHC-2 Mk.III Turbo Beaver, an advanced turboprop conversion of de Havilland Canada's legendary bush plane, represented the ultimate evolution of one of aviation's most capable STOL aircraft. First flown in 1947 as the original DHC-2, the Mk.III variant entered production in the late 1960s with a powerful Pratt & Whitney Canada PT6 turboprop engine producing 578 equivalent horsepower. This high-wing, single-engine aircraft could carry up to 2,600 pounds of useful load while maintaining the exceptional short-field performance that made the Beaver series indispensable to bush pilots across Canada's remote territories. Only 60 Mk.III Turbo Beavers were manufactured by De Havilland Canada before production ended in 1967.

Design Origins and Development

The foundation for the Mk.III Turbo Beaver was established on September 17, 1946, when de Havilland Canada assembled a design team consisting of Fred Buller, Dick Hiscocks, Jim Houston, and Wsiewołod Jakimiuk under the leadership of Phil Garratt. Their mission was to create what would become known as a "half-ton, flying pickup truck" capable of operating from land, water, or snow. The original DHC-2 prototype took its maiden flight on August 16, 1947, launching a program that would ultimately produce 1,657 aircraft across all variants.

The Manufacturer's Legacy

De Havilland Canada, based in Downsview, Ontario, was still under British ownership when the Beaver project began. The company's innovative approach to bush aircraft design earned recognition in 1987 when the Canadian Engineering Centennial Board named the DHC-2 as one of the top ten Canadian engineering achievements of the 20th century. Today, Viking Air of British Columbia holds all original patents and continues to service existing aircraft while producing parts and new examples of the larger Otter series.

Turboprop Transformation

The Mk.III variant represented a radical departure from the original design's Pratt & Whitney R-985 Wasp Junior radial engine. Engineers installed a Pratt & Whitney Canada PT6A-6 or PT6A-20 turboprop engine, delivering 431 kilowatts or 578 equivalent horsepower. This powerplant transformation required significant airframe modifications, including a 28-inch fuselage extension aft of the pilot's seat to maintain proper center of gravity balance. The additional power also necessitated a larger rudder and enlarged vertical fin to manage the increased torque and performance capabilities.

The turboprop conversion resulted in a nearly 400-pound increase in maximum gross weight, enabling a useful load of 2,600 pounds. This enhancement made the Mk.III particularly attractive to operators requiring maximum payload capacity while retaining the exceptional STOL characteristics that defined the Beaver series.

Limited Production Run

During the late 1960s, de Havilland Canada produced exactly 60 Mk.III Turbo Beavers before ceasing all DHC-2 production in 1967. This limited run contrasted sharply with the success of the original Mk.I variant, of which the United States military alone purchased 968 to 970 aircraft designated as U-20 utility transports during the Korean War era. The first production Beaver had been delivered in April 1948 to the Ontario Department of Lands and Forests, who had participated as a design partner throughout development.

Bush Flying Excellence

The Turbo Beaver became the preferred aircraft among bush pilots serving Canada's remote northern territories, accessing locations previously reachable only by canoe or on foot. Its design incorporated practical features for harsh operating conditions, including an oil reservoir filler located in the cockpit, allowing pilots to add oil during flight—a critical capability for aircraft operating in extreme cold and remote locations far from maintenance facilities.

The aircraft's construction utilized steel components from the engine to the firewall, heavy aluminum truss frames with panels and doors throughout the front section, and progressively lighter structures toward the rear with full monocoque construction aft. This engineering approach provided exceptional durability while maintaining optimal weight distribution.

Continuing Legacy

Despite production ending in 1967, hundreds of DHC-2 Beavers remain active worldwide, many extensively modified to incorporate modern technology and meet evolving operational requirements. Kenmore Air of Kenmore, Washington, has become synonymous with Beaver restoration and modification, holding dozens of supplemental type certificates for aircraft improvements. Rebuilt aircraft from this facility are commonly known as "Kenmore Beavers" and feature zero-hour fatigue-life ratings.

Aviation historian Neil Aird of Kingston, Ontario, has dedicated considerable effort to researching and documenting the fate of every DHC-2 ever constructed, testament to the aircraft's enduring significance in aviation history. The Beaver's reputation as a Canadian aviation icon reflects its unmatched capability in serving remote communities and supporting resource extraction industries across the country's vast wilderness areas.

Beyond the factory Mk.III variant, numerous aftermarket conversions have emerged, including the Wipaire Boss Turbo-Beaver and the Airtech Canada DHC-2/PZL-3S, which utilizes current-production PZL-3S radial engines producing 600 horsepower. These modifications demonstrate the continued relevance of the basic Beaver design nearly eight decades after its initial conception.