Douglas DC-4E
Technical Specifications
| First Flight: |
June 7, 1938 |
| Number Built: |
1as prototype |
| Length: |
97 feet 7 inches |
| Wing Span: |
138 feet 3 inches |
| Height: |
24 feet 6.5 inches |
| Max Take-Off Wt.: |
66,500 lbs. |
| Max Landing Wt.: |
61,500 lbs. |
| Empty Wt.: |
42,564 lbs. |
| Max Speed: |
245 mph 213 kts |
| Normal Cruising Speed: |
200 mph 173 kts |
| Service Ceiling: |
22,900 feet |
| Fuel Capacity: |
N/A |
| Range: |
2200 miles |
| Fuel Type: |
100/130 octane |
| Fuel Consumption: |
N/A |
| Engines: |
4 Pratt & Whitney R-2180-S1A1-G
rated @ 1450 HP each |
| Seating: |
52 Passengers |
| Crew: |
2 Pilots and 2 Flight Attendents |
|
Engine Specifications
|
|
Pratt & Whitney R-2180-S1A1-G
|
| Type: |
14 cylinder air cooled radial |
| Diameter: |
N/A |
| Length: |
N/A |
| Bore: |
N/A |
| Stroke: |
N/A |
| Displacement: |
2180 cubic inches |
| Compression Ratio: |
N/A |
| Dry Weight: |
N/A |
| Ignition: |
N/A |
| Fuel Grade: |
100/130 octane |
| Carburation: |
N/A |
| Performance: |
Take-Off 1450 HP |
|