Chapter 12 - Fuel Flashcards
Centre fuel tank fuel is used before main tank fuel because:
Centre tank fuel pumps produce higher pressure than main tank pumps
The fuel quantity indication system calculates:
Usable fuel quantity in each tank.
The capacity of the centre fuel tank is:
Greater than the capacity of the two main fuel tanks combined.
No 1 & 2: 4,876 / each
Centre: 16,273
There are CDS fuel alert indications for:
3x - two mains, one centre.. think Fuel L.I.C for the lights..
- Main tank - fuel quantity less than 2000 lbs. (907 kg.) “LOW”. Displayed until 1134kg in the tank
- Main tanks - greater than 1000 lbs. (453 kg.) fuel difference “IMBAL”. Displayed until less than 91kg difference
- Centre tank - greater than 1600 lbs. (726 kg.) and both switches turned off “CONFIG”. Displayed until 363kg in tank, engines off, one pump switch on.
During cruise, both centre tank fuel pumps have failed and the centre tank fuel pump switches are OFF. You still have 700 lbs. (320 kg.) of fuel in the centre tank and both main tanks are full.
The Upper Display Unit will show:
a. LOW indication - 2000 lbs (907kg) in main tank but mains are full
b. a CONFIG indication - greater than 1600 lbs. (726 kg.) and both CTR fuel pump switches turned off but CTR has 320kg.
c. a pump LOW PRESSURE indication - only activates with pump switches on and they’re off
d. None of the answers are correct.
D - none
You have 5,500 lbs. (2500 kg.) of fuel in the No 1 main tank and 6750 lbs. (3060 kg.) of fuel in the No.2 main tank.
You will see:
An IMBAL indication below main tank No.1 with no Master Caution light and no system annunciation for fuel.
In flight, below FL300, two fuel pump LOW PRESSURE lights for the No.1 tank illuminate.
What happens to the No.1 engine?
It will continue to operate. Mechanical engine-driven fuel pumps provide suction feed
in the event that normal electrical fuel pump operation is not available.
The centre tank scavenge jet pump operates when:
The No.1 main fuel tank is about 1/2 full and the main tank No.1 forward pump is operating.
In which fuel tanks are bypass valves located?
Both main tanks.
What is the condition of the VALVE OPEN light when the cross feed selector is positioned OPEN and the cross feed valve is closed?
Illuminated bright blue.
What is the source of electrical power for the engine fuel shutoff valves?
The Battery Bus.
Ground transfer of fuel between the tanks:
is accomplished at the wing fuelling station.
During fuel balancing operations, fuel pump pressure should be supplied at all times.
Without fuel pump pressure, thrust deterioration or engine flameout may occur above which altitude?
30,000 feet.
If the fuel quantity indication system is inoperative:
Enter and periodically update manually calculated fuel weight on the FMC PERF INIT page.
What causes the ENG VALVE CLOSED lights to illuminate bright blue?
When the valve is in transit or valve position and engine start lever or engine fire warning switch disagree.
What is the power source for opening and closing the SPAR FUEL SHUTOFF VALVES?
DC power from the Hot Battery Bus
Where is the fuel temperature sensor located?
In Main Tank number 1
What is the maximum tank fuel temperature?
49 degrees C.
What is the minimum in-flight tank fuel temperature?
-43 degrees C or 3 degrees C above freezing point of fuel being used. Whichever is
higher
What causes the Crossfeed VALVE OPEN light to illuminate bright blue?
Crossfeed valve is in transit or valve position and crossfeed selector disagree
When must the crossfeed valve be closed?
for takeoff and landing.
What powers the crossfeed valve?
DC power so with complete loss of AC power, fuel can be directed to both engines from any tank.
What causes the FILTER BYPASS light to illuminate?
Impending fuel filter bypass due to a contaminated filter
What causes the centre tank fuel pump LOW PRESSURE light to illuminate?
Fuel pump output pressure is low with the FUEL PUMP switch ON.
What causes the centre tank fuel pump LOW PRESSURE light to extinguish?
Centre tank FUEL PUMP switch OFF, or FUEL PUMP switch ON and output pressure is normal.
How is the centre tank fuel pump LOW PRESSURE light different from the main tank fuel pump LOW PRESSURE lights?
Main tank fuel pump LOW PRESSURE lights illuminate when output pressure is low, regardless of switch position.
The centre wing tank fuel scavenge jet pump transfers fuel remaining in the centre wing into
which main tank?
Number 1 main tank
When AC fuel pumps are not operating, fuel for the APU is suction fed from which tank?
Number 1 main tank.
What does an illuminated main tank fuel pump LOW PRESSURE light indicate?
Fuel pump switch is OFF and /or the fuel pump output pressure is low.
What powers the centre wing and main tank fuel pumps?
AC powered. Therefore with a complete loss of AC power, the engines are being suction fed
What is the defueling valve used for?
The defueling valve, located outboard of the number 2 engine, is used for defueling and tank to tank transfer operation
Can tank-to-tank transfer of fuel be accomplished in flight?
No.
Which fuel tank pumps produce greater pressure?
Centre wing tanks produce greater pressure overriding the main tank pumps in the fuel manifold. Therefore the centre wing fuel will be used to pressure feed the engines before the main tank fuel is used.