Loading...
Lockheed Loadstar 2019-07-03T14:55:08-05:00

Project Description

MPH

266

WEAPONS

0

SEATS

20

Lockheed Loadstar

Role:  Passenger transport

National Origin: United States

Manufacturer: Lockheed

First Flight: 1940

Primary User: United States Army Air Corps

Number Built: 625

Sales of the 10–14 passenger Lockheed Model 14 Super Electra, which first flew in 1937, had proved disappointing, despite the aircraft’s excellent performance, as it was more expensive to operate than the larger Douglas DC-3, already in widespread use. In order to improve the type’s economics, Lockheed decided to stretch the aircraft’s fuselage by 5 feet 6 inches (1.68 m), allowing an extra two rows of seats to be fitted.

The prototype for the revised airliner, designated Model 18 by Lockheed, was converted from the fourth Model 14, one of a batch which had been returned to the manufacturer by Northwest Airlines after a series of crashes. The modified aircraft first flew in this form on September 21, 1939, another two prototypes being converted from Model 14s, with the first newly built Model 18 flying on February 2, 1940.

When the United States started to build up its military air strength in 1940–41, many American-operated Lodestars were impressed as the C-56. This was followed by the construction of many new-build Lodestars which were flown by the U.S. Army Air Forces as the C-60 and by the U.S. Navy and U.S. Marine Corps as the R5O. Lend-lease aircraft were used by the RNZAF as transports.

General characteristics

  • Crew: 2
  • Capacity: 18 passengers
  • Length: 49 ft 10 in (15.19 m)
  • Wingspan: 65 ft 6 in (19.96 m)
  • Height: 11 ft 10 in (3.6 m)
  • Wing area: 551 ft² (51.2 m²)
  • Empty weight: 12,500 lb (5,670 kg)
  • Loaded weight: 17,500 lb (7,938 kg)
  • Max. takeoff weight: 21,000 lb (9,825 kg)
  • Powerplant: 2 × Wright R-1820-56S nine-cylinder air-cooled radial engines, 1,350 hp  each

Performance

  • Maximum speed: 266 mph (231 knots, 428 km/h) at 17,150 ft (5,230 m)
  • Cruise speed: 200 mph (174 knots, 322 km/h)
  • Range: 2,500 mi (2,174 nmi, 4,025 km)
  • Service ceiling: 25,400 ft (7,740 m)
  • Climb to 10,000 ft (3,050 m): 6.6 minutes