|
Variant |
DC-6 |
DC-6A |
DC-6B |
Crew |
Three to Four |
Capacity |
48-68 Passengers |
28,188 lb (12,786 kg) of Cargo |
42-89 Passengers |
Length |
100 ft 7 in (30.66 m) |
105 ft 7 in (32.18 m) |
Wingspan |
117 ft 6 in (35.81 m) |
Height |
28 ft 5 in (8.66 m) |
Wing Area |
1,463 sq ft (135.9 m2) |
Empty weight |
52,567 lb (23,844 kg) |
45,862 lb (20,803 kg) |
55,357 lb (25,110 kg) |
Max takeoff weight |
97,200 lb (44,100 kg) |
107,200 lb (48,600 kg) |
107,000 lb (49,000 kg) |
Powerplant (4x) |
Pratt & Whitney R-2800-CA15
"Double Wasp" radial engine,
1,800 hp (1,300 kW) with
water injection each
|
Pratt & Whitney R-2800-CB16
"Double Wasp" radial engine,
2,400 hp (1,800 kW) each |
Pratt & Whitney R-2800-CB17
"Double Wasp" radial engine,
2,500 hp (1,900 kW) each |
Propellers |
Hamilton Standard 43E60 "Hydromatic" constant-speed
props with autofeather and reverse thrust |
Cruise speed |
311 mph (501 km/h) |
315 mph (507 km/h) |
Fuel Capacity |
4,260 US gallons (16,125 litres)
4,722 US gallons (17,874 litres) |
|
up to 5,512 US gallons (20,865 litres) |
Range |
3,983 nmi (7,377 km) |
2,948 nmi (5,460 km) Max payload
4,317 nmi (7,995 km) Max fuel |
2,610 nmi (4,830 km) Max payload
4,100 nmi (7,600 km) Max fuel |
Service ceiling |
|
21,900 ft (6,700 m) |
25,000 ft (7,600 m) |
Rate of climb |
1,070 ft/min (330 m/min) |
|
|
|
Role |
Airliner/transport aircraft |
Manufacturer |
Douglas Aircraft Company |
First flight |
February 15, 1946 |
Introduction |
March 1947 |
Status |
Out of production, in limited use |
Primary users |
Pan American World Airways
Northwest Orient Airlines
Capital Airlines
Delta Air Lines |
Produced |
1946 - 1958 |
Number built |
704 |
Developed from |
Douglas DC-4 |
Variants |
Douglas DC-7 |
|
|
|
|
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