Editing Avionics (section)

===Fuel Systems===
Fuel Quantity Indication System (FQIS) monitors the amount of fuel aboard. Using various sensors, such as capacitance tubes, temperature sensors, densitometers & level sensors, the FQIS computer calculates the mass of fuel remaining on board.

Fuel Control and Monitoring System (FCMS) reports fuel remaining on board in a similar manner, but, by controlling pumps & valves, also manages fuel transfers around various tanks.

* Refuelling control to upload to a certain total mass of fuel and distribute it automatically.
* Transfers during flight to the tanks that feed the engines. E.G. from fuselage to wing tanks
* Centre of gravity control transfers from the tail (trim) tanks forward to the wings as fuel is expended
* Maintaining fuel in the wing tips (to alleviate wing bending due to lift in flight) & transferring to the main tanks after landing
* Controlling fuel jettison during an emergency to reduce the aircraft weight.