Lockheed Model 12 Electra Junior

Airplanes

Length

10.9728 m

Flat Wing Span

14.9352 m

Height

2.7432 m

Flat Wing Area

32.7019 m²

Max Seating

Cruise Speed

342.7903 km/h

Max Speed

362.1024 km/h

Max Ceiling

6979.92 m

Number of Engines

First Flight

1936-06-27

Number Built

130

Maximum Take-Off Weight

3.9236 t (paragliders: kg)

Maximum Range

1287.475 km

Pictures

No pictures yet for this family.

Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Maximum Range (km)
Lockheed Model 12 Electra Junior	3.9236	1287.475

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)	Max Seating
Beechcraft Queen Air	Lycoming O-540	10.668	15.24	9	Compare
Dornier Do 28	Lycoming O-540	11.41	15.55	12	Compare
Scaled Composites Triumph	Williams FJ44	11.8872	14.6304		Compare
Airspeed Consul		10.668	16.1544		Compare
Kawasaki Ki-45		11	15.02		Compare
AeroVolga LA-8		10.8	15	7	Compare

All data (22 fields)

Name: Lockheed Model 12 Electra Junior
Manufacturer: Lockheed Corporation
Description: 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.
First Flight: 1936-06-27
Designer: Lockheed Corporation
Type: Civil and military utility aircraft
Length (m): 10.9728
Height (m): 2.7432
Cockpit Crew: 2
Max Seating: 6
Max Speed (km/h): 362.1024
Cruise Speed (km/h): 342.7903
Max Ceiling (m): 6979.92
Rate of Climb (m/s): 7.112
Capacity Description: 6 passengers
National Origin: United States of America
Number Built: 130
Powerplant Description: 2 × Pratt & Whitney R-985 Wasp Junior SB 9-cylinder air-cooled radial engines, 336 kW (450 hp) each
Wikipedia Article (URL): en.wikipedia.org/wiki/Lockheed_Model_12_Electra_Junior
Flat Wing Span (m): 14.9352
Flat Wing Area (m²): 32.7019
Number of Engines: 2