Lockheed L-188 Electra
Airliner
Photo ©: Mike Vallentin
The Lockheed L-188 Electra is a four-engine short- to medium-range turboprop airliner for up to 99 passengers produced by the US-American manufacturer Lockheed Corporation. Many Electra had been converted as cargo freighters after their service as airliners.
Propulsion | 4 Turboprop Engines |
Engine Model | Allison 501D-13 |
Engine Power (each) | 2796 kW | 3750 shp |
max. Cruise Speed | 600 km/h | 324 kts 373 mph |
max. Speed (vne) | 674 km/h | 364 kts 419 mph |
Service Ceiling | 9.144 m | 30.000 ft |
Range | 3.541 km | 1.912 NM 2.200 mi. |
Empty Weight | 26.036 kg | 57.400 lbs |
max. Takeoff Weight | 51.256 kg | 113.000 lbs |
Wing Span | 30,18 m | 99 ft 0 in |
Wing Area | 120,8 m² | 1300 ft² |
Length | 31,85 m | 104 ft 6 in |
Height | 10,01 m | 32 ft 10 in |
First Flight | 06.12.1957 |
Production Status | out of production |
Production Range | 1958-1961 |
Total Production | 170 |
ICAO Code | L188 |
IATA Code | LOE LOF LOM |
FAA TCDS | 4A22 |
Data for (Version) | Lockheed L-188A Electra |
Variants | L-118A, L-188C |