341-350

Question 1

Do not reset a tripped fuel pump or fuel pump control circuit breaker.
a)
True
b)
False

Answer 1

true

Question 2

In flight tank fuel temperature must be maintained at least ______ above the fuel freezing point of the fuel being used.
a)
3°C
b)
5°C
c)
10°F

Answer 2

3°C

Question 3

Main wing tanks must be scheduled to be full if the center wing tank contains more than 1000 pounds of fuel.
a)
True
b)
False

Answer 3

True

Question 4

With center tank fuel, use center tank fuel for all operations with all operable boost pumps _____ and the CROSSFEED valve _____ until center tank fuel is depleted.
a)
OFF; closed
b)
ON; open
c)
ON; closed

Answer 4

ON; closed

Question 5

With no center tank fuel, use main tank-to-engine fuel feed with all operable main tank boost pump _____, center tank boost pump _____, and the CROSSFEED valve _____.
a)
ON; ON; open.
b)
ON; OFF; closed.
c)
OFF; ON; closed.

Answer 5

ON; OFF; closed

Question 6

Both center tank fuel pump switches must be positioned OFF when:
a)
the first center tank fuel pump LOW PRESSURE light illuminates if the center tank is empty.
b)
when established in a level flight altitude, if the center tank contains useable fuel.
c)
if the center tank fuel quantity exceeds 1000 pounds.

Answer 6

the first center tank fuel pump LOW PRESSURE light illuminates if the center tank is empty.

Question 7

Positioning the ENG 1 hydraulic pump switch to OFF isolates fluid flow from the system components and the pump ____ to rotate.
a)
ceases
b)
continues

Answer 7

continues

Question 8

If a leak develops in the A system hydraulic electric motor-driven pump or its related lines:
a)
a standpipe in the reservoir prevents a total system fluid loss
b)
the quantity in the reservoir steadily decreases to zero and all system pressure is lost
c)
The system quantity will steadily decrease to 15%

Answer 8

the quantity in the reservoir steadily decreases to zero and all system pressure is lost

Question 9

The purpose of the PTU is to supply the additional volume of hydraulic fluid needed to operate the autoslats or the leading edge flaps and slats at the normal rate when:
a)
the standby system volume is lost
b)
system A engine-driven pump volume is lost
c)
system B engine-driven pump volume is lost

Answer 9

system B engine-driven pump volume is lost

Question 10

The purpose of the landing gear transfer unit is to raise the landing gear at the normal rate when:
a)
system A engine-driven pump volume is lost due to a #1 engine failure
b)
the standby system volume is lost
c)
system B engine-driven pump volume is lost due to a #2 engine failure

Answer 10

system A engine-driven pump volume is lost due to a #1 engine failure