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Gulfstream 200 > SELF-CHECK 4 / HYDRAULICS/LANDING GEAR/BRAKES (Ch. 15) > Flashcards

SELF-CHECK 4 / HYDRAULICS/LANDING GEAR/BRAKES (Ch. 15) Flashcards

1
Q

Which grouping contains entirely hydraulic subsystems?

A. Gear, Q-feel spring, wheel brakes, slats
B. Air brakes, nosewheel steering, thrust reversers, slats
C. Krueger fl aps, stick pusher, thrust reversers, slats
D. None of the above

A

D. None of the above.

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2
Q

The G200 has how many electric motor pumps for moving hydraulic fluid?

A. One
B. Two
C. Three
D. Four

A

A. One.

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3
Q

Are the G200 hydraulic systems independent of each other?

A. Yes
B. No

A

A. Yes.

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4
Q

Which of the following are powered by both hydraulic systems?

A. Krueger flaps and stick pusher
B. Air brakes and thrust reversers
C. Ailerons and elevators
D. None of the abov

A

C. Ailerons and elevators.

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5
Q

Which of the following are powered by the left hydraulic system?

A. Left thrust reverser, emergency brakes, outboard airbrakes
B. Right thrust reverser, emergency brakes, outboard airbrakes
C. Wheel brakes, landing gear, Q-feel spring
D. Stick pusher, landing gear, outboard airbrakes

A

A. Left thrust reverser, emergency brakes, outboard airbrakes.

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6
Q

How can the pilot set the parking brake without starting an engine?

A. Turn on the electric motor pump
B. Motor the left engine
C. Use a hydraulic accumulator
D. The pilot cannot set the parking brake without starting an engine

A

A. Turn on the electric motor pump.

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7
Q

What is normal hydraulic pressure?

A. 2,250 PSI to 3,250 PSI
B. 2,500 PSI to 3,000 PSI
C. 2,700 PSI to 3,250 PSI
D. 3,000 PSI to 3,500 PSI

A

C. 2,700 PSI to 3,250 PSI.

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8
Q

Which hydraulic system does the electric motor pump serve?

A. Left
B. Right
C. Both
D. Nitrogen accumulator

A

B. Right.

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9
Q

Which system does the emergency landing gear extension use?

A. Left hydraulic system
B. Right hydraulic system
C. Stored pneumatic pressure (nitrogen)
D. None of the above

A

C. Stored pneumatic pressure (nitrogen).

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10
Q

Emergency braking is available using which system(s)?

A. A hydraulic accumulator
B. Left hydraulic system
C. Right hydraulic system
D. Either A or B

A

A. A hydraulic accumulator.

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11
Q

With the switch set to “AUTO,” under what circumstances will the electric motor pump automatically operate?

A. Either main landing gear not locked up with one thrust lever set beyond MAX CLIMB
B. Low pressure in the left hydraulic system (below 1,200 PSI)
C. Low pressure in the right hydraulic system (below 1,200 PSI)
D. Both A and C

A

D. Both A and C.

Either main landing gear not locked up with one thrust lever set beyond MAX CLIMB.

Low pressure in the right hydraulic system (below 1,200 PSI).

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12
Q

With a total loss of hydraulic power, the airplane is unflyable.

A. True
B. False

A

B. False.

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13
Q

At what airspeed does the Q-feel system begin to operate?

A. 100 KIAS
B. 125 KIAS
C. 150 KIAS
D. 200 KIAS

A

C. 150 KIAS.

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14
Q

How many accumulators are installed in the G200 hydraulic system?

A. One
B. Two
C. Three
D. Four

A

C. Three.

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15
Q

What does the left hydraulic accumulator provide?

A. One left T/R deployment and stow
B. Parking brakes
C. Six applications of emergency brakes for a total of 50 seconds
D. Either A or C

A

D. Either A or C.

One left T/R deployment and stow
or
Six applications of emergency brakes for a total of 50 seconds

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16
Q

With the pedestal switch in the OVRRD position, the electric motor pump will run even when the thermal protection would otherwise turn the pump off due to high load.

A. True
B. False

A

A. True.

17
Q

What is the approximate normal pressure for the emergency landing gear nitrogen bottle?

A. 1,000 PSI
B. 2,000 PSI
C. 3,000 PSI
D. 4,000 PSI

A

C. 3,000 PSI.

18
Q

What is the correct hydraulic accumulator nitrogen pre-charge pressure?

A. 1,000 PSI
B. 1,150 PSI
C. 600 PSI
D. 1,250 PSI

A

D. 1,250 PSI.

19
Q

What does the L HYD LEVEL LOW message mean?

A. Hydraulic fluid level in left reservoir is high
B. Hydraulic fluid level in left reservoir is low
C. Both A and B
D. The FQMS has malfunctioned

A

B. Hydraulic fluid level in left reservoir is low.

20
Q

What does the AUX HYD PRESS LOW message mean?

A. Pressure is below 6 PSI
B. The electric motor pump switch is in the “OFF” position
C. Hydraulic pressure is low and the pump is on
D. None of the above

A

D. None of the above.

21
Q

When will the crew receive a HYD PUMP PRESS HI message?

A. Hydraulic pressure above 3,250 PSI
B. Hydraulic pressure above 3,500 PSI
C. Hydraulic pressure above 3,750 PSI
D. None of the abov

A

B. Hydraulic pressure above 3,500 PSI.

22
Q

When will the crew receive a L HYD QTY REFILL message?

A. In-flight with Hydraulic fluid quantity in left reservoir less than 90%
B. On the ground with Hydraulic fluid quantity in left reservoir less than 90%
C. On the ground with Hydraulic fluid quantity in left reservoir less than 80%
D. Both A and B

A

B. On the ground with Hydraulic fluid quantity in left reservoir less than 90%.

23
Q

How can the landing gear be lowered with right hydraulic system failure?

A. Activate the emergency landing gear extension handle near the pilots right knee
B. Use the left hydraulic system
C. Use the nitrogen bottle installed for the purpose
D. Both A and C

A

D. Both A and C.

Activate the emergency landing gear extension handle near the pilots right knee.

Use the nitrogen bottle installed for the purpose.

24
Q

The landing gear may be retracted once they have been extended with the emergency extension system.

A. True
B. False

A

B. False.

25
Q

What can the pilot do if the landing gear handle will not move up?

A. Recycle the handle down then back up
B. Apply steadily increasing pressure
C. Press and hold the DOWNLOCK OVERRIDE button while raising the landing gear handle
D. None of the above

A

C. Press and hold the DOWNLOCK OVERRIDE button while raising the landing gear handle.

26
Q

What does the GEAR NOT DOWN message mean?

A. Landing gear is not down and locked with radar altitude of less than 800 feet
B. One thrust lever at or below max cruise detent or flaps more than 25º
C. None of the above
D. Both A and B required

A

D. Both A and B required.

Landing gear is not down and locked with radar altitude of less than 800 feet AND
One thrust lever at or below max cruise detent or flaps more than 25º.

27
Q

The emergency braking system is just as effective as the normal breaking system.

A. True
B. False, only half as effective

A

B. False, only half as effective.

28
Q

At what speed is the anti-skid system deactivated?

A. Below 25 kts
B. Below 15 kts
C. Below 10 kts
D. Below 5 kts

A

C. Below 10 kts.

29
Q

When is braking available?

A. Not until after touchdown and wheel spin-up above 25 kts
B. Not until after touchdown and wheel spin-up above 35 kts
C. Not until after touchdown and wheel spin-up above 15 kts
D. Immediately upon touchdown

A

B. Not until after touchdown and wheel spin-up above 35 kts.

30
Q

Which antiskid light is also the antiskid on/off switch?

A. The one on the right
B. The one on the left
C. Both
D. It depends upon airplane serial number

A

B. The one on the left.

31
Q

What controls are powered by the right hydraulic system?

A

GQBRINKS – Gear, Q-feel, Brakes, Right T/R, Inboard Spoilers, Nose Wheel Steering, Kreugers, Stick Pusher.

32
Q

What controls are powered by the left hydraulic system?

A

LEO - Left T/R, Emergency Brakes, Outboard Spoilers.

33
Q

On which side is the aileron autopilot servo? On which side is the elevator autopilot servo?

A

Left Aileron & Right Elevator.

34
Q

Is braking power available with complete hydraulic failure?

A

Yes, limited braking is available from the left accumulator and parking brake is available from the right accumulator.

35
Q

What is clean-wing maximum landing weight in view of maximum tire speed?

A

26,000 pounds

Gulfstream 200 (22 decks)

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