Convair 110
Technical Specifications
| First Flight: |
July 8, 1946 |
| Number Built: |
1 was built as a proto-type for the Convair 240 |
| Length: |
71 feet |
| Wing Span: |
89 feet |
| Height: |
25 feet 2.5 inches |
| Max Take-Off Wt.: |
35,970 lbs. |
| Max Landing Wt.: |
N/A |
| Empty Wt.: |
21,100 lbs. |
| Maximum Speed: |
314 mph 273 kts |
| Normal Cruising Speed: |
260 mph 226 kts |
| Approach Speed: |
N/A |
| Landing Speed: |
N/A |
| Stall Speed: |
79 mph 68 kts |
| Service Ceiling: |
N/A |
| Fuel Capacity: |
N/A |
| Range: |
560 miles |
| Fuel Type: |
100/130 octane |
| Fuel Consumption: |
N/A |
| Engines: |
2 Pratt & Whitney R-2800 SC13G |
| Seating: |
30 Passengers |
| Crew: |
2 Pilots and 1 Flight Attendent |
|
Engine Specifications
|
|
R-2800
SC13G
|
| Type: |
18 cylinder air cooled radial |
| Diameter: |
52.8 inches |
| Length: |
81.4 inches |
| Bore: |
5.75 inches |
| Stroke: |
6 inches |
| Displacement: |
2804 cubic inches |
| Compression Ratio: |
6.75 to 1 |
| Dry Weight: |
2390 lbs. |
| Ignition: |
Scintilla DLN-10 low tension |
| Fuel Grade: |
100/130 octane |
| Carburation: |
Stromberg PR-58E5 |
| Performance: |
Rated @ 2100 HP each for take-off |
|