Increased size, gross weight and engine power of Super VC10, compared with standard VC10 now flying, led to fin torsion box structure being constructed as integral fuel tank; component is built by Sud-Aviation at its St. Nazaire plant in France; fuel tank capacity is 1340 Imperial gal; fuel is transferred by gravity feed into wing center section tank and pumped to main system in wings for delivery to engines; details of construction of fin torsion box and fuel tank and fuel system layout are shown diagrammatically.


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    Titel :

    Super VC10 fin fuel system


    Weitere Titelangaben:

    Aircraft Eng


    Erschienen in:

    Erscheinungsdatum :

    1964


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Super VC10

    Harrison, N.F.G. | Engineering Index Backfile | 1965


    The Super VC10

    Emerald Group Publishing | 1965


    Flying super VC10

    Nicholl, J. | Engineering Index Backfile | 1965


    Introduction to super VC10

    Engineering Index Backfile | 1965


    Interior engineering and super VC10

    Barfield, N.A. | Engineering Index Backfile | 1965