Fuel

Question 1

True or False: There is a gravity refuel port for each wing tank.

Answer 1

True

Question 2

Where is the port for pressure-refueling located?

Answer 2

Right #2 Engine nacelle

Question 3

True or False: There is engine fuel cross-feed capability on the aircraft..

Answer 3

False

Question 4

True or False: Even though there is not cross-feed capability, pilots can still transfer fuel between the main tanks.

Answer 4

True

Question 5

Fuel burn rate for the Q400 is measured in which of the following units?

Answer 5

PPH

Question 6

Each fuel tank has how many sections?

Answer 6

3

Question 7

True or False: The surge bay is used primarily for venting the main tank.

Answer 7

True

Question 8

What is the total useable fuel from the tanks in pounds?

Answer 8

11,724

5862 a side.

Question 9

What is the maximum lateral fuel imbalance allowed between tanks in flight?

Answer 9

600 lbs.

Question 10

When are the auxiliary fuel pumps required to be selected ON?

Answer 10

Takeoff

Landing

Primary Ejector
pump failure

Fuel Xfer

Question 11

How many scavenge pumps are there in each wing?

Answer 11

4

Question 12

How many scavenge pumps are there on the aircraft in total?

Answer 12

8

Question 13

True or False: The scavenge pumps are powered using motive flow.

Answer 13

True

Question 14

True or False: The APU fuel shutoff valve is controlled automatically by the fire protection system.

Answer 14

True

Question 15

If certain fuel information becomes invalid or unavailable, how is that indicated in the flight deck?

Answer 15

White dashes replace the digits or dials

Question 16

If any fuel quantity computer fails, what is used to determine the fuel quantity?.

Answer 16

Magnetic sticks

Question 17

True or False: Fuel can be transferred between tanks in flight..

Answer 17

True

Question 18

True or False: Fuel can be transferred between tanks on the ground.

Answer 18

True, Whenever 115v A/C power is available

Question 19

When the inlet fuel temperature is in the normal range, what color is it displayed in on the ED?

Answer 19

White

Question 20

When the inlet temperature is below 0 degrees C, what color is it displayed in on the ED?

Answer 20

Amber

Question 21

When the inlet temperature is above 71 degrees C, what color is it displayed in on the ED?

Answer 21

Red

Question 22

Where is the REFUEL/DEFUEL control panel located?

Answer 22

Door at the bottom of #2 engine nacelle

Question 23

The Fuel system is able to accomplish which of the following?

Answer 23

Transfer between tank

Question 24

Which of the following is not a component of the fuel tanks?

Answer 24

…

Question 25

The primary ejector pumps are powered by _____..

Answer 25

Motive flow

Question 26

The purpose of scavenge pumps is to _____..

Answer 26

Deliver fuel from the low points of the tank to the collector box

Question 27

If pilots needed to transfer fuel from Tank 1 to Tank 2, which Aux pump would be used?

Answer 27

Tank #2

Question 28

True or False: With no power applied to the aircraft, the aircraft cannot be refueled.

Answer 28

Tank 1

Question 29

What quantity of fuel in the tank will cause the Tank Fuel Low caution light to illuminate?

Answer 29

~305 lbs. in either tank

Question 30

True or False: With no power applied to the aircraft, the aircraft cannot be refueled.

Answer 30

False