Where are fuel quantities displayed?
Where is the fuel temperature displayed?
Do all the fuel pumps have the same pressure output?
With all tanks full and pumps operating, which tank supplies the engines?
From which tank can fuel be jettisoned?
Where can the jettison time be observed?
On ground with only 1 electric power source, how will the tank pumps operate during engine start?
What is indicated if the cross-feed switch valve light remained illuminated after selection during manual operation?
Where can the fuel freeze temperature be entered?
What will happen when the actual temperature approaches the preset fuel freeze temperature?
Where is the DC fuel pump located?
When does the DC pump operate on ground?
What will cause the DC pump to automatically shut down?
If a main fuel pump fails, will selecting the pump switch off remove the message and light?
Is the engine operation affected by a tank pump off?
To what quantity will fuel be automatically jettisoned?
Can all the fuel be jettisoned?
Describe the fuel balance system.
When is fuel balance operation inhibited?
When will the FMC show a FUEL DISAGREE message?
FUEL DISAGREE advisory is displayed when a discrepancy between the FQIS totalizer fuel quantity and the FMC-calculated fuel quantity is equal to or more than 2,268 Kg or (5000 lb) continuously for 5 minutes.
WT787-14 - Page 4 (787 WingTIPs)
What is the nitrogen generation system?
It generates nitrogen enriched air to displace fuel vapors in all fuel tanks. This air minimizes fuel flammability during normal flight and ground operations.
If there is fuel in the centre tank, and centre tanks pumps fail, is the fuel unusable?