351-360

Question 1

If a leak develops in either pump, line, or component of System B:
a)
the quantity in the reservoir steadily decreases to approximately zero, system B pressure and the standby system pressure is lost
b)
the quantity in the reservoir steadily decreases to approximately zero and system B pressure is lost, however the power transfer unit is still operational
c)
The system quantity will steadily decrease to 15%

Answer 1

the quantity in the reservoir steadily decreases to approximately zero and system B pressure is lost, however the power transfer unit is still operational

Question 2

The standby system _______ and uses a single electric motor-driven pump.
a)
can only be activated by placing the ALTERNATE FLAPS Master Switch to ARM
b)
can be activated manually or automatically
c)
can only be activated by positioning either FLIGHT CONTROL switch to STBY RUD

Answer 2

can be activated manually or automatically

Question 3

Pulling an engine fire warning switch shuts off the hydraulic fluid flow to the related engine-driven pump and:
a)
engages the standby hydraulic system
b)
deactivates the ENG # hydraulic LOW PRESSURE light
c)
activates the ENG # hydraulic LOW PRESSURE light

Answer 3

deactivates the ENG # hydraulic LOW PRESSURE light

Question 4

The landing gear transfer unit operates when airborne, the No. 1 engine RPM drops below a limit value, ______________.
a)
the landing gear is positioned up, and either main landing gear is not up and locked
b)
the landing gear is positioned up, and both main landing gear are not up and locked
c)
and a main landing gear is not up and locked

Answer 4

the landing gear is positioned up, and either main landing gear is not up and locked

Question 5

Automatic operation of the standby hydraulic pump is initiated when loss of hydraulic system A or B, and:
a)
flaps extended; and airborne, or wheel speed greater than 60 knots
b)
flaps retracted and airborne
c)
all answers are correct

Answer 5

flaps extended; and airborne, or wheel speed greater than 60 knots

Question 6

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

Answer 6

a standpipe in the reservoir prevents a total system fluid loss

Question 7

_______ hydraulic system is capable of providing full power control to the ailerons.
a)
Only the A
b)
Only the B
c)
Either

Answer 7

Either

Question 8

The aircraft has ______ hydraulic systems.
a)
two
b)
three
c)
four

Answer 8

three

Question 9

______ can power all flight controls with no decrease in aircraft controllability.
a)
The RAT
b)
The standby hydraulic system
c)
Either A or B hydraulic system

Answer 9

Either A or B hydraulic system

Question 10

Normal operating pressure for each hydraulic system is ______ psi.
a)
2,000
b)
3,000
c)
3,500

Answer 10

3,000