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