FUEL SYSTEM GENERALTHE standard version or the F.28 has a conventional two-tank fuel system with an integral tank in each outer wing section contained by the wing torsion box with a total capacity of 2,170 Imp. gal. or 17,200 lb. of fuel. The centre wing torsion-box pro-vides space for additional bladder type tanks with a capacity varying from 312 to 700 Imp. gal. or 2,460 to 5,500 lb. as desired.


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    Title :

    Aircraft Systems


    Subtitle :

    Details of the fuel system, the auxiliary power unit, hydraulic, flight controls, air conditioning and pressurisation systems, with details of the electrical system and avionics



    Publication date :

    1967-07-01


    Size :

    11 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English



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