Lockheed Model 12 Electra Junior
| Model 12 Electra Junior | |
|---|---|
 |
|
| French-registered Lockheed 12A F-AZLL | |
| Role | Civil and military utility aircraft |
| Manufacturer | Lockheed Corporation |
| First flight | June 27, 1936 |
| Number built | 130 |
| Developed from | Lockheed Model 10 Electra |
The Lockheed Model 12 Electra Junior, more commonly known as the Lockheed 12 or L-12, is an eight-seat, six-passenger all-metal twin-engine transport aircraft of the late 1930s designed for use by small airlines, companies, and wealthy private individuals. A scaled-down version of the Lockheed Model 10 Electra, the Lockheed 12 was not popular as an airliner but was widely used as a corporate and government transport. Several were also used for testing new aviation technologies.
After Lockheed had introduced its 10-passenger Model 10 Electra, the company decided to develop a smaller version which would be better suited as a "feeder airliner" or a corporate executive transport. At the same time, the U.S. Bureau of Air Commerce had also sensed the need for a small feeder airliner and announced a design competition for one. In order for a candidate to qualify for the competition, a prototype had to fly by June 30, 1936.
Lockheed based its candidate, which it named the Model 12 Electra Junior, around a smaller, improved version of the Electra airframe. It would carry only six passengers and two pilots but would use the same 450 hp (340 kW) Pratt & Whitney R-985 Wasp Junior SB radial engines as the main Electra version, the 10A. This made it faster than the Electra, with a top speed of 225 mph (362 km/h) at 5,000 ft (1,500 m). Like the Electra, the Model 12 had an all-metal structure, trailing-edge wing flaps, low-drag NACA engine cowlings, and two-bladed controllable-pitch propellers (later changed to constant-speed propellers). It also had the Electra's twin tail fins and rudders, which were becoming a Lockheed trademark. The landing gear was a conventional tail-dragger arrangement, with the main wheels retracting backwards into the engine nacelles; as was often the case with retractable gear of the period, the wheel bottoms were left exposed in case a wheels-up emergency landing was necessary.
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