Viscount 700
Technical Specifications
| First Flight: |
July 16, 1948 |
| Number Built: |
445 were built for commercial use |
| Length: |
81 feet 9 inches |
| Wing Span: |
93 feet 8 inches |
| Height: |
27 feet 9 inches |
| Max Take-Off Wt.: |
64,500 lbs. |
| Max Landing Wt.: |
60,285 lbs. |
| Empty Wt.: |
36,112 lbs. |
| Maximum Speed: |
310 mph 269 kts |
| Max Cruising Speed: |
272 mph 237 kts |
| Normal Cruising Speed: |
264 mph 230 kts |
| Approach Speed: |
165 mph 144 kts |
| Landing Speed: |
140 mph 122 kts |
| Stall Speed: |
N/A |
| Service Ceiling: |
25,000 feet |
| Fuel Capacity: |
2,309 US gallons |
| Water Methanol Capacity: |
132 US gallons |
| Range: |
1,500 miles |
| Fuel Type: |
Jet A |
| Fuel Consumption: |
268 gph 4 engine flight plan burn |
| Engines: |
4 Rolls-Royce Dart 510 Turbo-Prop |
| Seating: |
48 Passengers |
| Crew: |
2 Pilots and 2 Flight Attendents |
|
Engine Specifications
|
|
Rolls
Royce Dart 510
|
| Type: |
Axial-Flow Prop-Jet |
| Diameter: |
N/A |
| Length: |
N/A |
| Compressor Stages: |
N/A |
| Turbine Stages: |
N/A |
| Weight: |
N/A |
| Starter: |
Air Frame furnished |
| Fuel Grade: |
JP-4 or Jet A |
| Estimated Shaft HP: |
1,600 SHP @ 14,500 rpm take-off
1,365 SHP @ 14,000 max continuous power |
|