Brainscape's Knowledge GenomeTM

Browse over 1 million classes created by top students, professors, publishers, and experts.


See full index

Gulfstream 200 > SELF-CHECK 4 / FUEL (Ch. 14) > Flashcards

SELF-CHECK 4 / FUEL (Ch. 14) Flashcards

1
Q

Pouring undiluted fuel additive into the fuel tanks is an approved practice.

A. True
B. False

A

B. False

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
2
Q

How many fuel tanks are installed on the G200?

A. Five
B. Six
C. Seven
D. Eight

A

C. Seven

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
3
Q

What is the last fuel tank before the fuel is sent to the engine ?

A. Wing
B. Forward
C. Fuselage
D. Feed

A

D. Feed

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
4
Q

How are the feed jet pumps for each engine powered ?

A. Electrically
B. Hydraulics
C. By motive flow
D. There are no feed jet pumps

A

C. By motive flow.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
5
Q

With the switch in “AUTO” position, when does the standby fuel pump operate?

A. Fuel pressure drops below 6 PSI
B. Fuel pressure drops below 4 PSI
C. None of the above
D. Both A and B

A

A. Fuel pressure drops below 6 PSI.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
6
Q

From which engine feed line does the APU receive its fuel supply?

A. The left engine
B. The right engine
C. Both A and B
D. None of the above

A

B. The right engine.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
7
Q

How is fuel delivered to the feed tanks?

A. Jet pumps
B. Gravity
C. Both A and B
D. None of the above

A

C. Both A and B.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
8
Q

The fuel usage and transfer sequence is as follows: upper portion of the fuselage tank, forward tank, lower portion of the fuselage tank, center tank, wings tanks and the feed tanks.

A. False
B. True

A

B. True.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
9
Q

How is fuel balanced using the active balance method?

A. Gravity
B. Standby fuel pumps
C. Both A and B
D. None of the above

A

B. Standby fuel pumps.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
10
Q

How is fuel balanced using the wing interconnect method?

A. Gravity
B. Standby fuel pumps
C. Both A and B
D. None of the abov

A

A. Gravity.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
11
Q

When is fuel jettison from each feed tank stopped automatically?

A. When the feed tank quantity drops below 130 lbs
B. When the JETTISON switch is turned off manually
C. When the respective wing tank fuel quantity drops below 600 lbs
D. All of the above

A

D. All of the above.

When the feed tank quantity drops below 130 lbs.
When the JETTISON switch is turned off manually.
When the respective wing tank fuel quantity drops below 600 lbs

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
12
Q 
When total fuel quantity is below \_\_\_\_\_ lbs, it is recommended that only one jettison valve be opened, not two, and that the WING INTERCONNECT valve be opened.
A. 3,000
B. 4,000
C. 5,000
D. 6,000
A

C. 5,000.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
13
Q

Each feed tank holds ___ lbs of fuel.

A. 100
B. 200
C. 710
D. 170

A

D. 170.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
14
Q

The G200 fuel tanks hold aggregate _____ lbs of fuel.

A. 14,500
B. 13,500
C. 15,020
D. 15,200

A

C. 15,020.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
15
Q

What does the Fluid Quantity Measurement System (FQMS) measure?

A. Fuel quantity, Fuel flow, Fuel temperature in the right wing
B. APU and Engine oil level
C. Hydraulic reservoirs fluid level
D. All of the above

A

D. All of the above

Fuel quantity, Fuel flow, Fuel temperature in the right wing.
APU and Engine oil level.
Hydraulic reservoirs fluid level.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
16
Q

What is the function of the cockpit pedestal REFUEL OFF pushbutton?

A. Stops pressure refueling from the cockpit
B. Defuels the airplane
C. Both A and B
D. None of the above

A

A. Stops pressure refueling from the cockpit.

17
Q

Under what circumstances will the crew receive a FEED TANK FUEL LOW message?

A. Fuel quantity below 1,500 lbs
B. Fuel quantity below 300 lbs
C. Feed tank fuel quantity below 300 lbs
D. Feed tank fuel quantity below 130 lbs

A

D. Feed tank fuel quantity below 130 lbs.

18
Q

Under what circumstances will the crew receive a FUEL
PUMP INOP message?

A. Fuel standby pump is operative
B. FUEL PUMP switch is ON
C. Fuel standby switch in ON/AUTO with low fuel pressure
D. All of the abov

A

C. Fuel standby switch in ON/AUTO with low fuel pressure

19
Q

What does a L FUEL FILTER message mean?

A. Left fuel filter is clogged
B. Right fuel filter is clogged
C. Both A and B
D. None of the above

A

A. Left fuel filter is clogged.

20
Q

What does a FUEL WING UNBAL message mean?

A. Asymmetry between left and right wing fuel quantity greater than 600 lbs
B. Asymmetry between left and right wing fuel quantity greater than 300 lbs
C. Asymmetry between left and right wing fuel quantity greater than 400 lbs
D. Asymmetry between left and right wing fuel quantity greater than 500 lbs

A

B. Asymmetry between left and right wing fuel quantity greater than 300 lbs.

21
Q

What does a FUEL LEVEL LOW message mean?

A. Fuel level in both wing tanks is less than 300 lbs (approx. 960 lbs total)
B. Fuel level in either wing tank is less than 300 lbs (approx 960 lbs total)
C. Fuel level in the forward fuselage is less then 300 lbs (approx 960 lbs total)
D. None of the abov

A

B. Fuel level in either wing tank is less than 300 lbs (approx 960 lbs total).

22
Q

The development of what particular problem may be indicated by a FUEL XFER ABNORMAL message?

A. CG may shift beyond forward limit
B. Fuel temperature may rise
C. Passengers may become ill
D. CG may shift beyond aft limit

A

D. CG may shift beyond aft limit.

23
Q

When will the crew receive a FUEL PUMP ON message?

A. Fuel pressure drops
B. STBY FUEL PUMP switch is in the ON position
C. Fuel jettison or balance pushbutton is pressed
D. All of the above

A

D. All of the above.

Fuel pressure drops
STBY FUEL PUMP switch is in the ON position.
Fuel jettison or balance pushbutton is pressed

24
Q

Under what circumstances may the crew receive a FUEL LEAK message?

A. Anytime fuel consumption indicates an apparent leak
B. In cruise flight when fuel consumption indicates an apparent leak
C. When APU fuel consumption indicates an apparent leak
D. On ground only

A

B. In cruise flight when fuel consumption indicates an apparent leak.

25
Q

What condition will cause a FUEL TANK TEMP LOW message?

A. Heat exchanger bypass
B. Fuel temperature too low for selected fuel type
C. Outside air temperature below ISA -25
D. Icing condition

A

B. Fuel temperature too low for selected fuel type.

26
Q

Short Answer

What is motive flow?

A

Motive flow is fuel flow resulting when excess fuel at the engines is routed at high pressure to jet pumps. These jet pumps cause the fuel to move throughout the system on the basis of Bernoulli’s principle:
If a small amount of fluid is flowing horizontally from a region of high pressure to a region of low pressure, then there is more pressure behind than in front. This results in application of force on the fluid, propelling it forward.

27
Q

With a BOW of 20,500 lbs, is it possible to carry a 1,000 lbs payload and full tanks without exceeding a weight limitation?

A

No.

Gulfstream 200 (22 decks)

Brainscape helps you reach your goals faster, through stronger study habits.
© 2024 Bold Learning Solutions. Terms and Conditions