Lockheed Model 18 Lodestar Civil Aircraft Model Details

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General Information of Lockheed Model 18 Lodestar

Developed From : Lockheed Model 14 Super Electra

First Flight : September 21, 1939

Introduction : March 30, 1940

Manufacturer : Lockheed

National Origin : United States

Number Built : 625[1]

Primary Users : United States Army Air Corps

Role : Passenger transport

Variants : Lockheed Ventura

General characteristics of Lockheed Model 18 Lodestar

Capacity : 18 passengers

Crew : 3

Empty Weight : 12,500 lb (5,670 kg)

Height : 11 ft 10 in (3.6 m)

Length : 49 ft 10 in (15.19 m)

Loaded_Weight : 17,500 lb (7,938 kg)

Max Takeoff Weight : 21,000 lb (9,825 kg)

Powerplant : 2 × Wright R-1820-87 nine-cylinder air-cooled radial engines, 1,200 hp (895 kW) each

Wing Area : 551 ft² (51.2 m²)

Wingspan : 65 ft 6 in (19.96 m)

Performance of Lockheed Model 18 Lodestar

Cruise Speed : 200 mph (174 knots, 322 km/h)

Maximum Speed : 266 mph (231 knots, 428 km/h) at 17,150 ft (5,230 m)

Range : 2,500 mi (2,174 nmi, 4,025 km)

Service Ceiling : 25,400 ft (7,740 m)

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