end of lesson questions

Question 1

______ pumps are installed in the center hydraulic system.

Answer 1

4

Question 2

Hydraulic reservoirs are pressurized by:

Answer 2

Bleed air

Question 3

Left and right engine driven pumps operate continuously, while the left and right electric pumps operate on-demand.

Answer 3

True

Question 4

The left hydraulic system normally powers:

Answer 4

Flight Controls

Right Yaw Damper

Question 5

Hydraulic fluid is cooled by:

Answer 5

Fuel tank heat exchangers

Question 6

What displayed hydraulic quantity will result in a refill (RF) message, indicating that the reservoir should be refilled?

Answer 6

.75 or less

Question 7

Pump low pressure indications are inhibited when the associated pump is selected OFF.

Answer 7

False

Question 8

The pitch enhancement system (PES) supplies power to:

Answer 8

Stabilizer trim

Question 9

When will the QTY light illuminates on the Hydraulic Panel and the EICAS advisory message L, R or C HYD QTY displays

Answer 9

quantity is .50 or less,

Question 10

What would cause an IDG to disconnect? Choose all correct answers.

Answer 10

GEN DRIVE DISC switch pushed

Thermal disconnect on some a/c

Question 11

Power from the generator is routed to the main AC bus through the generator control breaker.

Answer 11

true

Question 12

Which items are powered by the main AC buses?

Answer 12

utility and galley buses
flight instrument transfer buses
TRUs

Question 13

What can power the ground handling bus?

Answer 13

external power

APU

Question 14

The ground service bus can be powered on the ground and in flight.

Answer 14

true

Question 15

What items will shed when the first engine start selector is moved to the GND position?

Answer 15

both utility buses

Question 16

If the center hydraulic system fails, the right autopilot will:

Answer 16

not be affected

Question 17

LNAV will activate immediately when selected with the airplane within ___ NM of the route.

Answer 17

2.5

Question 18

True or False: Once the autothrottles have been disconnected with the A/T disconnect switches on the thrust levers, the A/T ARM switch must be cycled to rearm the autothrottle.

Answer 18

false

Question 19

Which is the FMA indication that the go-around mode is armed?

Answer 19

there is no FMA indication that GA is armed

Question 20

What stations can be connected through the flight interphone system?

Answer 20

ground crew at nose

all flight deck postions