Lockheed L-188
Technical Specifications
| First Flight: |
December 12, 1957 |
| Number Built: |
222 for Commercial & Military service |
| Length: |
116 feet 10 inches |
| Wing Span: |
99 feet 8 inches |
| Height: |
33 feet 8 inches |
| Max Take-Off Wt.: |
113,000 lbs. |
| Max Landing Wt.: |
N/A |
| Empty Wt.: |
61,491 lbs. |
| Max Cruising Speed: |
448 mph 389 kts |
| Normal Cruising Speed: |
373 mph 324 kts |
| Stall Speed: |
N/A |
| Service Ceiling: |
28,400 feet |
| Fuel Capacity: |
5520 US gallons |
| Range: |
2200 miles |
| Fuel Type: |
Jet A |
| Fuel Consumption: |
935 gph 4 engines flight plan burn |
| Engines: |
4 Allison 501-D13D rated @ 3750 eshp each |
| Seating: |
99 to 127 Passengers |
| Crew: |
2 Pilots 1 Flight Engineer and 3 Flight Attendents |
Engine Specifications
|
Allison
501-D13
|
| Type: |
Axial-flow prop-jet |
| Diameter: |
27 inches |
| Length: |
145 inches |
| Compressor Stages: |
14 |
| Turbine Stages: |
4 |
| Weight: |
1750 lbs. |
| Starter: |
Air-frame furnished |
| Fuel Grade: |
Jet A |
| Estimated Shaft Horse Power: |
3750 @ 13,820 rpm |
|