Passenger Turbo Props
Douglas DC-6
ICAO: DC6
Overview
The Douglas DC-7 was produced by the Douglas Aircraft Company introduced on November 29, 1953. It was the final transport aircraft powered by a piston engine built by the company between 1953 to 1958.
Live Fleet Activity (DC7)
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Specifications
Units
- Engine
- 4 × Wright R3350
- Engine type
- Piston
- Power
- 4 × 3,250 hp · 2,424 kW
- Avionics
- —
- Wing tips
- No winglets
- Seats
- 78
- Crew
- —
- Cabin width
- —
- Cabin height
- —
- Cabin length
- —
- Exterior length
- 108 ft 1 in · 32.95 m
- Tail height
- 28 ft 8 in · 8.75 m
- Fuselage diameter
- 10 ft 6 in · 3.20 m
- Wing span
- 117 ft 5 in · 35.80 m
- Baggage volume
- —
- Gross weight
- —
- Empty weight
- —
- Max takeoff weight
- 116,500 lb · 53,000 kg
- Max landing weight
- 97,000 lb · 44,000 kg
- Max payload
- 20,800 lb · 9,450 kg
- Fuel capacity
- 4,500 gal · 17,100 L · 12,300 kg (AvGas)
- Max cruise speed
- 347 kt · 399 mph · 643 km/h
- Maximum speed
- —
- Cruise speed
- —
- Approach speed
- 84 kt · 97 mph · 156 km/h
- Range
- 2,606 nm · 3,000 mi · 4,830 km
- Fuel burn
- —
- Ceiling
- 25,000 ft · 7,600 m
- Rate of climb
- 1,200 ft/min · 6 m/s
- Takeoff distance
- 6,350 ft · 1,940 m
- Landing distance
- 5,250 ft · 1,600 m
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Operational Context
The DC-7 was developed out of the request of American Airlines for an aircraft that could fly the United States coast-to-coast in around eight hours nonstop. The aircraft manufacturer Douglas Aircraft Company was hesitant to produce the type until Cyrus Rowlett Smith, the CEO of American Airlines placed an order for twenty-five DC-7s costing $40 million which covered the development costs of the aircraft.
In May 1953, the prototype took to the air for the first time, and in November of the same year, the first DC-7 was delivered to American Airlines, starting the first east-coast-to-west-coast nonstop flight in the United States which led to the competitor Trans World Airlines to provide the same service with its Super Constellation aircraft.
The wing of the DC-7 was derived from the DC-4 and DC-6. It had the same wingspan of 35.81 meters and a wing area of 152.1 square meters. The fuselage was lengthened by 1 meter compared to the DC-6B, making it 34.21 meters, with a height of 8.75 meters, and a diameter of 3.2 meters.
The DC-7 was powered by four Wright R-3350 Duplex Cyclone Turbo-Compound engines. It is a twin-row, supercharged, air-cooled, radial engine with eighteen cylinders, pushrod valves, two-speed single-stage supercharger, Chandler-Evans downdraft carburetor fuel system, and dry-sump oil system. It produces a maximum thrust of 3,250 horsepower each.
The DC-7 produced different variants from the original DC-7 production type with 105 built, and the first long-range version DC-7B had 112 produced aircraft which were designed with a higher gross weight and an increase in fuel capacity. The DC-7C Seven Seas was a longer-range version capable of flying non-top in transatlantic routes. It was powered by more powerful R-3350 engines rated at 3,400 horsepower and added fuel capacity mostly in longer wings. A total of 121 DC-7Cs were built. The DC-7D was an unbuilt version intended to be powered by Rolls-Royce Tyne turboprop engines, and the DC-7F was a freight conversion equipped with two huge freight doors.