Flat Wing Area
120.774 m²
Flat Wing Aspect Ratio
7.5
Cruise Speed
600.2853 km/h
Entry Into service
1959-01-12
Maximum Take-Off Weight
51.2559 t (paragliders: kg)
Total Fuel Capacity
20895.47
Maximum Range
3540.557 km
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Aircraft Weight Variants
| Aircraft |
Maximum Take-Off Weight (t (paragliders: kg)) |
Total Fuel Capacity |
Maximum Range (km) |
|
Lockheed L-188 Electra |
51.2559 |
20895.47 |
3540.557 |
Similar airplanes
All data (29 fields)
- Name
- Lockheed L-188 Electra
- Manufacturer
- Lockheed Corporation
- Description
- The Lockheed L-188 Electra is an American turboprop airliner built by Lockheed.
- ICAO Code
- L188
- First Flight
- 1957-12-06
- Entry Into service
- 1959-01-12
- Production End
- 1961-01-01
- Designer
- Lockheed Corporation
- Type
- Turboprop airliner
- Length (m)
- 31.6992
- Height (m)
- 9.7536
- Max Seating
- 98
- Max Speed (km/h)
- 720.9861
- Cruise Speed (km/h)
- 600.2853
- Max Ceiling (m)
- 8656.32
- Rate of Climb (m/s)
- 10.0076
- Capacity Description
- ; 98 passengers or; 33800 lb payload
- National Origin
- United States of America
- Number Built
- 170
- Powerplant Description
- 4 × Allison 501-D13 turboprop engines, 2796 kW (3750 hp) each
- Primary Users
- Air Spray , Buffalo Airways, Conair Group (Retired) , Eastern Air Lines (Retired) , American Airlines (Retired) , National Airlines (Retired)
- Status
- In service as a cargo aircraft
- Wikipedia Article (URL)
- en.wikipedia.org/wiki/Lockheed_L-188_Electra
- Flat Wing Span (m)
- 30.1752
- Flat Wing Area (m²)
- 120.774
- Flat Wing Aspect Ratio
- 7.5
- Wake Category
- M
- Aircraft Engine
- Allison T56
- Number of Engines
- 4