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 |
|