Fuel Flashcards
How are the fuel tanks normally vented
The tanks are vented to atmosphere by 2 NACA scoops vents
Where is the aircraft fuel stored
In the two main wing tanks and one center collector tank
How are fuel system faults annunciated
Both a and b are correct: switch lights on the overhead fuel panel & on EICAS in the form of messages
What is used to provide the fuel system computer with fuel quantity information
Both a and b: six fuel quantity probes with compensator units in each of the main tanks & three probes in the center tank
How may the fuel level be manually checked on the ground
By means of magnetic level indicators
What type of ejector pumps are used to move fuel from main tanks to the collector tanks
Scavenge ejectors
What maintains fuel symmetry between the main tanks
Automatically controlled by the bi-directional x flow pump
How are the center collector tanks kept full
Gravity feed lines and scavenge ejectors
What is used to back up the main ejectors
Two electric boost pumps
The electric fuel boost pumps
All of the above: are energized during engine start, can feed fuel to either engine from one collector tank, back up the main ejector pumps
From what source is the APU fuel feed supplied
From left collector tank via APU fuel pump
Where is bulk fuel temperature taken
Right main wing tank
How is pressure refueling and suction refueling accomplished and how is it controlled
Accomplished through the single point refuel/defuel adapter. Controlled from the refuel/defuel control panel
If a fuel asymmetry condition exists between main tanks, what visual caution message is presented on EICAS
FUEL IMBALANCE
What fuel system information is displayed on the EICAS primary page
Individual tank quantities, total fuel quantity, fuel flow per engine