United States' Lockheed C-56 Lodestar, C-60 Lodestar transport
Design
The Lockheed Lodestar was developed from the Model 14 Super Electra and Hudson series.1,2 Initially produced as a civilian transport.1
Most airlines were going to buy the Douglas DC-3.1 There were 96 orders for export purchases.1 When the war started it was decided to be used by the military.1
Prototype
The Lodestar prototype first flew on September 21, 1939.1
The United States military ordered four planes in May 1941.2 In 1942 an order was placed for 325 C-60 Lodestars.2
Production
- Lockheed C-56: 11
- Lockheed C-57: 131
- Lockheed C-60A: 3251
- Lockheed R50-4: 121
- Lockheed R50-5: 411
- Lockheed R50-6: 351
- Total: 6251
Variants
- Lockheed C-56: US Army.3 Cyclone engines.1
- Lockheed C-57: US Army.3 Twin Wasp engines.1,3
- Lockheed C-59 / Lodestar Mk I: US Army.3
- Lockheed C-60 / Lodestar Mk II: US Army.3
- Lockheed C-60A: Major production version.1 Cyclone engines.1
- Lockheed C-66:
- Lockheed C-111:
- Lockheed R50: US Navy.3
- Lockheed R50-1: US Navy.1
- Lockheed R50-2: US Navy.1
- Lockheed R50-3: US Navy.1
- Lockheed R50-4: US Navy.1
- Lockheed R50-5: US Navy.1
- Lockheed R50-6: US Navy.1
Usage
The Lodestar was used by Australia, Britain, Netherlands, South Africa, and the United States.1
Start of World War II
The civilian versions of the Lodestar were requisitioned after the start of World War II.2
Britain
The Royal Air Force (RAF) used the Lodestar in four squadrons operating in the Middle East.1 They were used as transport and air ambulances.1
Specifications
| Lockheed Lodestar | Lockheed C-56 Lodestar | Lockheed C-60A | |
|---|---|---|---|
| Type | Transport1,3 | Transport2 | Transport1 |
| Crew | 2 - 32 | ||
| Passengers | 18: fully armed troops1 | 172 | 18: paratroopers1 |
| OR | 22: standard passengers1 | ||
| Payload | 5,000 lb3 | ||
| Engine (Type) | 2: Pratt & Whitney Twin Wasp3 2: Pratt & Whitney R-1690 Hornet1 |
2: Wright R-1820-71 Cyclone2 | |
| OR | 2: Wright R-1820 Cyclone1 | ||
| OR | 2: Pratt & Whitney R-1830 Twin Wasp1 | ||
| Cylinders | Cyclone: Radial 91 Wasp: Radial 141 |
Radial 92 | |
| Cooling | Air2 | ||
| HP | Hornet: 850 - 875 each1 Cyclone: 1,100 - 1,200 each1 Wasp: 1,050 each3, 1,200 each1 |
1,200 each2 | |
| Propeller blades | 3 each1 | ||
| Capacity | |||
| Dimensions | |||
| Span | 65' 6"1,3 19.96 m1 |
65' 6"2 | |
| Length | 49' 9"3, 49' 10"1 15.19 m1 |
49' 10"2 | |
| Height | 11' 10"1,3 3.61 m1 |
11' 1"2 | |
| Wing area | |||
| Weight | |||
| Empty | 12,075 lb1 5,477 kg1 |
||
| Loaded | 17,500 lb2 | 18,500 lb1 5,639 kg1 |
|
| Performance | |||
| Speed | 275 mph3 | 253 mph2 | |
| Speed @ 17,000' / 5,180 m |
266 mph1 428 kph1 |
||
| Cruising speed | 200 mph1 322 kph1 |
||
| Climb to 10,000 ' / 3,048 m |
6.6 minutes1 | ||
| Service ceiling | 23,300'2 | 30,000'1 9,144 m1 |
|
| Range | 1,700 miles3 | 1,600 miles2 | 1,660 miles1 2,671 km1 |
Sources:
- Aircraft of WWII, Stewart Wilson, 1998
- World War II Airplanes Volume 2, Enzo Angelucci, Paolo Matricardi, 1976
- Aeronautics Aircraft Spotters' Handbook, Ensign L. C. Guthman, 1943

