Overview
The de Havilland DHC-2 Beaver is a single-engine utility aircraft developed for rugged operations in remote regions. Designed in Canada after World War II, it became synonymous with bush flying. The aircraft’s versatility and short takeoff and landing performance made it a global workhorse.
Live Fleet Activity (DHC2)
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Specifications
Units
- Engine
- 1 × Pratt & Whitney R-985
- Engine type
- Piston
- Power
- 450 hp · 336 kW
- Avionics
- —
- Wing tips
- No winglets
- Seats
- 6
- Crew
- —
- Cabin width
- 4 ft 0 in · 1.22 m
- Cabin height
- 4 ft 3 in · 1.30 m
- Cabin length
- 9 ft 0 in · 2.74 m
- Exterior length
- 30 ft 3 in · 9.22 m
- Tail height
- 12 ft 2 in · 3.70 m
- Fuselage diameter
- 4 ft 3 in · 1.30 m
- Wing span
- 48 ft 0 in · 14.63 m
- Baggage volume
- —
- Gross weight
- —
- Empty weight
- —
- Max takeoff weight
- 5,100 lb · 2,300 kg
- Max landing weight
- —
- Max payload
- 2,100 lb · 950 kg
- Fuel capacity
- 140 gal · 500 L · 400 kg (AvGas)
- Max cruise speed
- 137 kt · 158 mph · 254 km/h
- Maximum speed
- —
- Cruise speed
- —
- Approach speed
- 45 kt · 52 mph · 83 km/h
- Range
- 395 nm · 450 mi · 730 km
- Fuel burn
- 2.84 nm/gal · 1.39 km/L
- Ceiling
- 18,000 ft · 5,500 m
- Rate of climb
- 1,020 ft/min · 5 m/s
- Takeoff distance
- 1,250 ft · 380 m
- Landing distance
- 1,250 ft · 380 m
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Live fleet activity details
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