Viscount 800
Technical Specifications
| First Flight: |
August 28, 1950 |
| Number Built: |
445 were built for commercial use |
| Length: |
N/A |
| Wing Span: |
N/A |
| Height: |
N/A |
| Max Take-Off Wt.: |
69,000 lbs. |
| Max Landing Wt.: |
62,000 lbs. |
| Empty Wt.: |
40,300 lbs. |
| Maximum Speed: |
340 mph 296 kts |
| Max Cruising Speed: |
307 mph 267 kts |
| Normal Cruising Speed: |
300 mph 260 kts |
| Approach Speed: |
152 mph 175 kts |
| Landing Speed: |
140 mph 122 kts |
| Stall Speed: |
N/A |
| Service Ceiling: |
25,000 feet |
| Fuel Capacity: |
2,288 US gallons |
| Water Methanol Capacity: |
132 US gallons |
| Range: |
2,000 miles |
| Fuel Type: |
JP-4 or Jet A |
| Fuel Consumption: |
346 gph 4 engine flight plan burn |
| Engines: |
4 Rolls-Royce Dart 525P Turbo-Prop |
| Seating: |
56 Passengers |
| Crew: |
2 Pilots and 2 Flight Attendents |
|
Engine Specifications
|
|
Rolls
Royce Dart 525P
|
| 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: |
1,730 SHP @ 15,000 rpm take-off
1,585 SHP @ 14,500 max continuous power |
|