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Gulfstream 200 > SELF-CHECK 5 / FLIGHT CONTROLS (Ch. 13) > Flashcards

SELF-CHECK 5 / FLIGHT CONTROLS (Ch. 13) Flashcards

1
Q

How can the crew disconnect the pitch control linkage between the pilot and copilot?

A. By steady alternating pushing and pulling of the control column
B. By striking either yoke with the crash axe
C. Both A and B
D. By pulling the PITCH lever in the left side pedestal

A

D. By pulling the PITCH lever in the left side pedestal.

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2
Q

After the PITCH handle has been pulled and the control columns have been unlinked, movement of the pilot’s yoke will move the _______ elevator(s).

A. Right
B. Left
C. Right and left
D. None of the above

A

B. Left.

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3
Q

After the ROLL handle has been pulled and the yokes are unlinked, the copilot’s yoke will control the aileron _______.

A. Right
B. Left
C. Center
D. None of the above

A

A. Right.

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4
Q

With a complete hydraulic system failure, can the crew unlink the yokes by pulling the ROLL handle?

A. Yes
B. No
C. Only when the PITCH handle also is pulled
D. Only in aircraft post-mod 10012, serial numbers 163 and subsequent

A

B. No.

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5
Q

How are the pilots’ rudder control inputs transferred to the rudder?

A. Fly by wire
B. Hydraulically
C. Through bell cranks, push-pull rods, and torque tubes
D. All of the above

A

C. Through bell cranks, push-pull rods, and torque tubes.

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6
Q

The rudder bias system is actuated by the differential bleed pressure during an asymmetric thrust condition.

A. True
B. False

A

A. True.

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7
Q

The elevator artifi cial feel system is comprised of a spring and an additional Q-feel unit for high speeds to change the control forces according to aircraft speed.

A. True
B. False

A

A. True.

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8
Q

It is normal to hear a tone while using primary pitch trim.

A. True
B. False

A

A. True.

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9
Q

The pitch trim has ___ independent electric systems for moving the stabilizer.

A. Two
B. Three
C. Four
D. None of the above

A

A. Two.

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10
Q

When is mach trim available?

A. When the autopilot is disengaged
B. When the ADC mach data indicates that longitudinal trim is necessary
C. Both A and B
D. None of the above

A

C. Both A and B.

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11
Q

How many channels does the pitch trim system have?

A. One
B. Two
C. Three
D. None of the above

A

B. Two.

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12
Q

What does pressing the PITCH TRIM REL button on either pilot’s yoke do?

A. Disconnect power from the trim unit primary channel
B. Powers up the secondary channel and the override switch
C. Disconnects the autopilot
D. All of the above

A

C. Disconnects the autopilot.

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13
Q

How does the pilot operate the secondary pitch trim system?

A. Move the HORIZ TRIM switch (located on the center pedestal) up or down
B. With the pitch trim switch on either yoke
C. Both A and B
D. None of the above

A

A. Move the HORIZ TRIM switch (located on the center pedestal) up or down.

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14
Q

How can the pilot restore the primary pitch drive system once it has been deactivated?

A. By pushing the pitch RESET pushbutton on the center pedestal
B. By double-clicking the PITCH TRIM REL. pushbutton on either control wheel
C. By restarting the airplane
D. None of the above

A

A. By pushing the pitch RESET pushbutton on the center pedestal.

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15
Q

How is aileron trim controlled?

A. On the pilots yoke
B. The trim switch on the center pedestal
C. On the copilots yoke
D. None of the above

A

B. The trim switch on the center pedestal.

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16
Q

How is rudder trim controlled?

A. On the pilots yoke
B. The trim switch on the center pedestal
C. On the copilots yoke
D. None of the above

A

B. The trim switch on the center pedestal.

17
Q

The copilot’s pitch trim switch has priority over the pilot’s.

A. True
B. False

A

B. False.

18
Q

How are the slats powered?

A. Hydraulically
B. Electrically
C. Pneumatically
D. None of the above

A

B. Electrically.

19
Q

How are the trailing edge fl aps powered?

A. Hydraulically
B. Electrically
C. Pneumatically
D. None of the above

A

B. Electrically.

20
Q

How are the Krueger flaps powered?

A. Hydraulically
B. Electrically
C. Pneumatically
D. None of the above

A

A. Hydraulically.

21
Q

Which of the following fl ight control surfaces extends first?

A. Slats
B. Trailing edge fl aps
C. Krueger fl aps
D. None of the above

A

A. Slats.

22
Q

Which of the following flight control surfaces retracts last?

A. Slats
B. Trailing edge fl aps
C. Krueger fl aps
D. None of the above

A

A. Slats.

23
Q

Is it OK to reverse your fl ap selection when the fl aps are still moving in the opposite direction?

A. Yes
B. It is not recommended
C. Never
D. Only until the fl aps extend 20 degrees

A

B. It is not recommended.

24
Q

If the slats did not fully extend, can the crew extend the flaps?

A. No
B. Yes, by selecting the SLAT BYPASS ARM pushbutton
C. Yes, by selecting the manual slat extension lever
D. Both B and C

A

B. Yes, by selecting the SLAT BYPASS ARM pushbutton.

25
Q

It is OK to use the SLAT BYPASS ARM pushbutton multiple times.

A. True
B. False

A

B. False.

26
Q

At what airspeed will a warning siren sound if the slats, flaps, and kruegers are not fully retracted?

A. 300 KIAS
B. 350 KIAS
C. 225 KIAS
D. Above 250 KIAS/0.55 M

A

D. Above 250 KIAS/0.55 M.

27
Q

What does a FLAP UNBAL message mean?

A. Asymmetry between left and right fl aps exceeds 1.2º
B. Asymmetry between the leading edge fl aps and the Krueger fl aps
C. Slats are not fully extended
D. Asymmetry between left and right fl aps exceeds 1.75 degrees

A

A. Asymmetry between left and right fl aps exceeds 1.2º.

28
Q

What four purposes does the Stall Protection and Q-feel system (SPQS) serve ?

A. Artificial feel, stall warning, maintain stall margin during icing, prevent stall with stick pusher
B. Stall warning, Artifi cial feel, auto hydraulic dump, stick pusher
C. Artifi cial feel, stall warning, maintain stall margin during icing, stick shaker
D. Auto hydraulic dump, stick pusher, stall warning, artificial feel

A

A. Artificial feel, stall warning, maintain stall margin during icing, prevent stall with stick pusher.

29
Q

What happens when a STALL message is displayed ?

A. Stick shaker activates and autopilot remainsconnected
B. Nothing yet
C. Stick shaker activates and disconnects the autopilot
D. Stick shaker activates only

A

C. Stick shaker activates and disconnects the autopilot.

30
Q

What message is displayed after a successful test of the SPQS?

A. SPQS Green
B. SPQS DONE
C. SPQS GOOD
D. SPQS TEST OK

A

D. SPQS TEST OK.

31
Q

Explain the “L A R E” acronym.

A

The aileron autopilot servo is on the left, and the elevator autopilot servo is on the right. This means that if an aileron jam is on the left side, the autopilot will be inoperative. Similarly, if an elevator jam is on the right side, the autopilot will be inoperative.

32
Q

With total hydraulic failure, can the crew disconnect the left and right ailerons using the ROLL disconnect handle?

A

No, the system is designed to prevent disconnection of the ailerons when there is complete hydraulic system failure.

33
Q

With total hydraulic failure, can the crew disconnect the left and right elevators using the PITCH” disconnect handle?

A

Yes.

34
Q

Is Mach trim available with the Auto Pilot OFF? With override trim?

A

Mach trim is available when the autopilot is OFF, but it is not available when the secondary pitch trim system is active.

35
Q

Does one control wheel pitch trim switch override the other?

A

Yes, the left side overrides the right.

36
Q

Which hydraulic system powers the inboard spoilers? Which powers the outboard spoilers?

A

The right hydraulic system powers the inboard (flight) airbrakes, and the left hydraulic system powers the outboard (ground) airbrakes.

37
Q

In the event of an engine failure what assists in rudder movement?

A

Bleed air from the operative engine.

38
Q

With total hydraulic failure, are the flaps and slats still operable? Kreugers?

A

The flaps and slats are electrically powered and are operative during hydraulic failure. The Kreuger flaps are hydraulically operated, so they would be inoperative during total hydraulic failure.

39
Q

With the flight airbrakes extended and hydraulic failure, what would happen to the airbrake panels?

A

They would “float” in the airstream.

Gulfstream 200 (22 decks)

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