Fuel Flashcards
The main ejectors:
A). Supply fuel to the APU
(B). Move fuel from the center tank to the wing tanks
(C). Provide fuel to the engines
(D). Provide motive flow for the scavenge and transfer ejectors
Provide fuel to the engines
The boost pumps move fuel from the:
(A). Center tank to the wing tank
(B). Collector tank to the engines
(C). Wing tank to the center tank
(D). Main ejectors to the engines
Collector tank to the engines
A FUEL IMBALANCE caution message will appear when an imbalance between wing tanks exceeds:
600
800
200
1,000
800 lbs
If the powered crossflow system fails, gravity crossflow can be used to _______ fuel balance
wing tank
center tank
maintain wing tank
In the event of an APU fuel pump failure:
(A). The APU will perform an auto shutdown
(B). The APU will continue to run using suction feed
(C). The APU will continue to run using fuel from the left main ejector
(D). The APU will shut down unless the left boost pump is manually selected on
The APU will continue to run using suction feed
Transfer ejectors are operated by:
electric boost pumps
motive flow
main ejectors
gravity feed
Motive flow
It provides the fuel required for combustion, control functions, motive flow and oil cooling:
the fuel control system
the FADEC
the fuel distribution system
the FMU
The fuel distribution system
The CRJ only has single point refueling capability.
t
f
False
The maximum usable fuel from a pressure refuel is ________ lbs.
14,810
17,492
19,594
21,374
19,594
From a pressure refuel the maximum fuel capacity of the CRJ is _______ lbs for the wing tanks and ________ lbs for the center tank.
6,992/5,610
7,992/3,610
7,405/4,610
7,492/4,610
7,492/4,610
The APU receives its fuel from the _____________ tank.
left collector
right right collector
center
scavenage
Left collector
Fuel is moved out of the wing tanks to the collector tanks by means of _________.
main ejectors
scavenge ejectros
transfer ejectors
the vent system
Scavenge ejectors
The engine fuel shutoff valves are controlled by:
A). The respective ENG STOP switchlight
B). The respective ENG START switchlight
C). The respective engine throttle
D). The ENGINE FIRE PUSH switchlight
The ENGINE FIRE PUSH switchlight
Automatic powered crossflow commences when a fuel imbalance of more than ________ lbs. exists between the wing tanks and stops when the low tank exceeds the other tank by _______ lbs.
200/50
500/100
300/100
200/100
200/50
Fuel transfer from the center tank to the wing tanks commences when a wing tank reaches _________ capacity.
85
94
90
87
94%
Takeoff with fuel in excess of ______ lbs. in the center tank is not permitted unless each wing tank quantity is above ________ lbs.
1000/4,400
750/5,300
1,000/4,950
500/4,400
500/4,400
Never remove the gravity filler caps if:
A). The boost pumps are on
B). The wing tanks are full or the fuel quantity is unknown
C). The APU is running
D). The BATT ESS BUS is powered by TRU1
The wing tanks are full or the fuel quantity is unknown
As an alternate method of measuring fuel tank quantity, the center tank has _________ magnetic fuel quantity indicator(s), while the wing tanks have __________.
2/1
1/3
1/2
2/3
1/2
Bulk fuel temperature readout measures the fuel temperature in the:
right wing tank
left wing tank
center tank
collector tanks
Right wing tank
Total fuel quantity turn amber when the quantity is ______ lbs. or less
600
1200
1600
1800
1200