Standard version of F.28 has conventional two-tank fuel system with integral tank in each outer wing section contained by wing torsion box with total capacity of 17,200 lb of fuel; details of fuel system, auxiliary power unit, hydraulic, flight controls, air conditioning and pressurization systems, with details of electrical system and avionics are presented; low weather minima approach system is based on automatic approaches during which ground guidance is Instrument Landing System followed by transition to manually controlled flight in all three axes at decision height and landing entirely by visual reference.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Aircraft systems


    Additional title:

    Aircraft Eng


    Published in:

    Publication date :

    1967


    Size :

    8 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




    Aircraft Systems

    Emerald Group Publishing | 1969


    Aircraft systems

    Moir, Ian / Seabridge, Allan G. | TIBKAT | 1992


    Aircraft Systems

    Renshaw, J.H. | Emerald Group Publishing | 1965


    Aircraft Systems

    Emerald Group Publishing | 1967


    Aircraft systems

    Pilʹa, Ján / Kozuba, Jarosław / Peruń, Grzegorz | TIBKAT | 2015