Overview
The Vickers Viscount 700 is a British medium-range turboprop airliner and the first production version of the Viscount suitable for operation through a range of climatic conditions, equipped with a pressurized fuselage, and can accommodate forty passengers and three crew members.
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Specifications
Units
- Engine
- 4 × Rolls-Royce RDa3
- Engine type
- Turboprop
- Power
- 4 × 1,381 shp · 1,030 kW
- Avionics
- —
- Wing tips
- No winglets
- Seats
- 32
- Crew
- —
- Cabin width
- 9 ft 5 in · 2.87 m
- Cabin height
- 5 ft 11 in · 1.80 m
- Cabin length
- 66 ft 11 in · 20.40 m
- Exterior length
- 81 ft 11 in · 24.96 m
- Tail height
- 26 ft 9 in · 8.16 m
- Fuselage diameter
- 10 ft 10 in · 3.29 m
- Wing span
- 93 ft 9 in · 28.58 m
- Baggage volume
- 530 ft³ · 15.0 m³
- Gross weight
- —
- Empty weight
- —
- Max takeoff weight
- 60,000 lb · 27,200 kg
- Max landing weight
- 58,500 lb · 26,600 kg
- Max payload
- 13,000 lb · 5,900 kg
- Fuel capacity
- 1,620 gal · 6,100 L · 4,900 kg (Jet A)
- Max cruise speed
- 276 kt · 318 mph · 511 km/h
- Maximum speed
- —
- Cruise speed
- —
- Approach speed
- 138 kt · 159 mph · 256 km/h
- Range
- 1,157 nm · 1,330 mi · 2,140 km
- Fuel burn
- —
- Ceiling
- 28,500 ft · 8,700 m
- Rate of climb
- 1,200 ft/min · 6 m/s
- Takeoff distance
- 5,050 ft · 1,540 m
- Landing distance
- 2,850 ft · 870 m
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