zoggavia
History of the Douglas DC-7
Project of a civil C-74
HP-379 HP-379, ex 42-65409, N3181G C-74 Heracles
at Turin, Italy, May 1967, Zoggavia Collection

When the development of the DC-7B was under way, Douglas realized the potential of the new 3 '400 hp version of the Wright R-3350 engine in manufacturing an even longer version of the DC-7 capable of flying the most important transatlantic routes non-stop in both directions and in all but the most adverse weather conditions. This ability was later used under the synonym 'Seven Seas', meaning all seas could be crossed non-stop.
N294 DC-7C leaving the Tokyo ramp
1960, Clinton H. Groves Collection
The fuel capacity was increased by an additional 5 foot (1,5 ) wing section inserted between the inboard engine and the wing root, thus giving the DC-7C an extra 10 foot (3m) wing span. This gave an additional capacity of 1'000 gallons (4'450 l) resulting in a range of 5'600 miles (9'000 km). A further 42 inch (1,06 m) fuselage ahead of the wings, and a taller fin and rudder to cope with the greater power and weight. The DC-7C's managed the a considerable share of the passenger traffic across the North Atlantic until the Boeing 707 and DC-8 jetliners were introduced in 1959 and 1960. Plans for a turboprop version, designated DC-7D, with Rolls Royce Tyne engines never materialized. All DC-7 built; 338 of all series.
DC-7C/F

| Versions |
C-74 |
DC-6B |
DC-7 |
DC-7B | DC-7C | DC-7C/F |
|
| Dimensions |
Length (m) |
37,58 | 32,50 | 29,53 | 33,98 | 34,21 | 34,21 |
| Wingspan (m) |
52,81 |
35,80 | 34,98 | 34,98 |
38,86 | 38,86 | |
| Height (m) |
13,34 | 8,78 |
8,75 |
8,75 |
9,70 |
9,70 |
|
| Wing Area (m2) |
233 | 188,3 |
188,3 | 197,04 |
197,04 |
191,30 |
|
| Weight |
Take off (t) |
78 |
48,5 | 57,2 |
57,2 | 57,2 |
57,2 |
| Fuel capacity (l) |
27'300 | 20'865 |
17'413 |
20'366 |
24'662 | 24'662 |
|
| Max Payload (t) |
21,3 | 9,1 |
9,1 | 9,8 |
10,4 | 15,9 | |
| Propulsion | Powerplant |
Pratt & Whitney R-4360-49 Wasp Major Radial |
Pratt & Whitney R-2800-CB17 Radial |
Wright R-3350 988TC-DA-2 Turbo compound radial |
Wright R-3350 988TC-DA-4 Turbo compound radial |
Wright R-3350 988TC-EA-4 Turbo compound radial |
Wright R-3350 988TC-EA-4 Turbo compound radial |
| Horsepower (hp) (kW) |
3'250 2'424 |
2'500 1'864 |
3'250 2'424 |
3'250 2'424 |
3'400 2'535 |
3'400 2'535 |
|
| Performance | Speed (km/h) |
528 | 507 | 503 |
504 |
563 |
563 |
| Range (km) |
8'350 - 12'550 |
4'200 - 8'014 |
41'00 - 6'067 |
4'587 - 6'880 |
6'437 - 7'890 |
6'437 - 7'890 |
|
| Passengers | 125 |
54-89 |
60-95 |
60-95 | 60-100 | 71-119 |
|
| First Flight |
Date | 5.9.45 |
2.2.51 | 18.5.53 |
21.4.54 | 20.12.55 | 27.6.1959 |
| First Service |
Date |
10.45 |
11.4.51 | 18.5.53 |
24.5.55 | 15.5.56 |
9.59 |
Military
French Air Force
DC-7 photo gallery - click the photo to enlarge