Systems-AFCS, Flight Controls, Flight Instruments Flashcards

1
Q

What is the primary purpose of the ALTITUDE pre-selector?

A

To command the aircraft to capture and maintain an altitude.

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2
Q

What happens when you push the XFER button on the flight control panel?

A

It couples the autopilot and the flight director to the other side.

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3
Q

When you press the XFR button what else should you also change?

A

The ATC SEL to coupled side

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4
Q

Does the autopilot disconnect when you push the SYNC button?

A

No, all you are doing is releasing the autopilot servo clutches.

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5
Q

What modes does the autopilot default to if no specific modes are selected?

A

The autopilot defaults to pitch and roll mode.

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6
Q

Does pressing the AFCS SEL switch from 1 to 1 change the flight director?

A

No, you get the same flight director but the backup FCC (flight control computer).

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7
Q

Which flight control surfaces does the autopilot trim?

A

Only the horizontal stab.

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8
Q

How many IRS systems are needed to engage the autopilot?

A

Two with independent sources for heading.

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9
Q

Describe the autopilot

A
  • Dual channel
  • Two-axis (pitch and roll)
  • Fail (passive)
  • Integrated with flight director
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10
Q

What is required to engage the autopilot?

A
  • two independent IRS sources
  • At least one yaw damper engaged (AP does not auto engage)
  • AP disconnect switch in normal position
  • No faults detected on act e FCCs
  • No excessive instability (pitch/roll/yaw rates or attitudes; G-load)
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11
Q

What does TURB mode do?

A

-Reduces pitch and roll gains of AP

Disconnects with AP disconnect, pushing of TURB button, or when capturing LOC.

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12
Q

Which hydraulic system operates the ground spoilers?

A

1 HYD system

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13
Q

Which side is the aileron A/P servo located?

A

Right side

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14
Q

When does the auto-ignition come on during the stall sequence?

A

When the needle on the SPS TEST gauge enters the BLUE area.

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15
Q

How is an aileron PCU JAM depicted on the FLT CTL synoptic page?

A

A “Half-Moon” symbol on the affected aileron.

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16
Q

What is the purpose of the flight spoiler detent mechanism?

A

To ensure a maximum “split” of 20degrees between sides.

17
Q

What is the significance of a “FLAP MOTOR OVERHEAT” message?

A

Flaps will move at half speed

18
Q

Which STAB TRIM channel is powered during EMER PWR only?

A

2 channel

19
Q

Which bus powers STAB TRIM channel #2?

A

DC ESS BUS

20
Q

What is the source for the LOW SPEED CUE?

A

AUX AOA vane

21
Q

What color is data that is pilot selected on the displays?

A

Magenta

22
Q

How can the TAKEOFF REF page be displayed?

A

Selecting the “MFD DATA” key on the CDU

23
Q

How does the EFIS display a failed source? (eg Altitude)

A

The failed information is removed and replaced by a red flag.

24
Q

What is the static source for the standby instruments?

A

The S3 ports (Below the pilot’s window)

25
Q

What is the DCP? Name something it controls.

A
  • Display Control Panel

- BRG Pointers; TERR/WX/TFC Overlays; MFD FRMT; NAV SRC

26
Q

How do you change the BARO setting scale from IN HG to HPGA?

A

HPA/IN tile on ADRP

27
Q

What does the AIRSPEED TREND VECTOR indicate?

A

What the airspeed will be in 10s at the present acceleration.

28
Q

The autopilot roll servo is connected to which side?

A

Co-pilot’s side

29
Q

How is the trim system prioritized?

A
  • Pilot
  • Co-Pilot
  • Autopilot
  • Mach
30
Q

When will FLT SPLR DEPLOY be indicated on EICAS?

A

Spoiler position is greater than 0 and:

  • RA 10-300ft
  • L or R engine N1 above 79%
  • RA inoperative and gear is down