Fuel Flashcards
How many fuel tanks and what are the approx. capacities?
7 tanks
CWT = 52.2 T (kg)
Main 2 and 3 = 38.1 T (each)
Main 1 and 4 = 13.3 T
Res 2 and 3 = 4.0T
What commands fuel valves to open or close and fuel pumps to turn on and off according to fuel management
logic?
FSMCs - Fuel System Management Cards
Which cross feed valves are affected by flap extension on the ground?
Xfeed 2 and 3 (allows for engines 2 + 3 to be fed by respective tanks. CWT feeds engines 1+4
Which fuel pumps are system logic pumps?
i.e which are commanded to turn on and off by system logic during normal operations?
Override/jettison fuel pumps 2+3
Trace fuel flow of fuel to engines when there are >7700kgs fuel in CWT from block out
- CWT pumps turned on - CTR tanks feed all engines
- Flaps extended - CTR tanks feed engine 1 and 4, main tanks 2 and 3 feed respective engines (Xfeed valves 2+3 auto-close)
- Flaps retracted - CTR tanks feed all engines (xfeed valves 2+3 auto-open)
- ‘FUEL LOW CTR’ - OVD pump 2 feeds eng 1 and 2, OVD pump 3 feeds eng 3 and 4
- ‘TANK/ENG’ - Each main tank pumps feed their engine (xfeed valves 1 and 4 turned off, OVD pumps 2+3 turned off)
When do the FSMCs open the reserve transfer valves
main tank 2 or 3 = 18,200kg
Under what conditions would fuel automatically transfer from main tanks 1 and 4 to their adjacent tanks 2 and 3
- During fuel jettison, when main tank 2 or 3 reach 9,072kg
- XFR valves 1 and 4 open and gravity feed
Can fuel be manually transferred from any tank to any other tank
No - no manual controls for reserve tank transfer
What occurs when Fuel Jettison Switch is selected to either A or B?
- arms jettison system
- displays preselected fuel to remain on EICAS
Describe how the fuel quantity indication changes upon termination of fuel jettison.
fuel to remain qty changes from magenta to white and flashes for 5 secs
What occurs when you push either fuel jettison nozzle valve to ON during the QRH fuel jettison procedure?
- jettison nozzle valve selected open
- when jettison system armed, activates override/jettison pumps in tanks containing fuel (pump switches must be ON)
What is the source of fuel for the APU?
- Main tank 2
- AC power available: aft boost pumps in main tank 2/3 supply pressure (3 operates to prevent tank-to-tank transfer, provides fuel if main pump 2 aft fails)
AC power not available: dedicated DC pump in main tank 2
In general, how are fuel imbalance situations handled?
- opening/closing x-feed valves + turning off and on fuel pump switches
- wait for EICAS - see FUEL BALANCING supp procedure
What is the impact on the aircraft of excessive fuel imbalance?
adversely affects CG, aerodynamic drag, and fuel
economy.
When is an engine on suction feed, and how are suction feed situations corrected?
- Main tank fuel pump pressure low, each engine can draw fuel from main tank through suction feed line bypassing pumps
- correct by open x-feed valves: fuel pressure can be provided from main tank with operating pumps to another engine