Aircraft Systems: 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

Abstract

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.

Citation

(1967), "Aircraft Systems: 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", Aircraft Engineering and Aerospace Technology, Vol. 39 No. 7, pp. 24-34. https://doi.org/10.1108/eb034282