Super G Characteristics
Technical characteristics
Year of construction: 1953
Manufacturer: Lockheed Aircraft Company - Burbank California -USA
Engines: Four Wright Cyclone 972 TC 18-DA3-Turbo compound 18-cylinder star-shaped engines, unit power 3250 hp, each driving a Hamilton 43 E 60-305 propeller - Diameter 4.62 m
Tanks : Fuel (7) 25 700 L or 6 550 gallons
Oil: 893 L or 227 gallons
Consumption: Fuel 1,800 l/h - Oil 40 to 60 l/h
Maximum speed : 595 Km/h at 20 000 feet
Cruising speed : 505 Km/h at 21 000 feet
Cruising altitude: 21,000 feet (6,300 m)
Equipped empty mass : 36 150 kg Max.
Take-off weight: 62,370 kg
Assignment: Air France Company
Registration: F-BGNJ
Commissioning: November 15, 1953
Accommodation: from 32 (Special Parisian) to 87 passengers (High Density)
10 crew members
Dimensions
Wingspan: 37,62 m
Length: 35,41 m
Height: 7,54 m
Wing area: 153,66 m2