Chapter 3: Automatic Flight Flashcards

1
Q

Bank Button

A

Limits bank to 17 degrees in HDG mode

(Post Mod LOAD 27.1) Limits bank to 15 degrees in HDG Mode

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2
Q

AFCS (Automatic Flight Control System) Components

A
  • Flight Director (FD)
  • Autopilot (AP) with coupled Go-Around (GA)
  • Yaw Damper (YD)
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3
Q

FD Automatically turns on when:

A
  • TO/GA button actuation
  • Manual selection of any vertical or lateral mode
  • AP engagement
  • WSHR Detection
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4
Q

To turn off the FD…

A

Press FD on the coupled side (with AP disengaged) to turn off both FDs.
OR…
Press FPA when FPA mode is already selected
*FD off => SpdT

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5
Q

Autopilot Non-normal and Abnormal Disengagement

A
  • AP is pressed on guidance panel
  • Either manual trim switch is pressed
  • Either stick shaker activated
  • Windshear escape guidance activated
  • Reversion of FBW to direct mode
  • Aileron or elevator disconnected
  • Pilot in put on control column; long-time light force, or short-time strong force
  • Internal monitor failure
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6
Q

Roll Mode Bank Limits

A

Current Bank < 6 degrees => commands wings level
6 degrees < Current Bank < 35 degrees => Maintains current bank
Current Bank > 35 degrees => Maintains 35 degrees

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7
Q

Takeoff Pitch Limits

A

For all engines operative: V2 + 10 kt
Failure below V2: V2
Failure between V2 and V2 + 10: Current Speed
Failure above V2 + 10: V2 + 10

TO pitch limited between 8 and 18 degrees
Max speed target VFE - 5
Min speed target VShaker + 10 (Vshaker + 3 for EO)

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8
Q

Go-Around Logic

A

Initially commands 8 degrees pitch to intercept speed target, then tracks speed
Speed Target:
-All engines, Vref + 20
-One engine, Vac
If speed target is invalid, commands 8 degrees pitch

Will not capture a selected altitude within 400’

GA pitch limited between 8 and 18 degrees
Max speed target VFE - 5
Min speed target VShaker + 10 (Vshaker + 3 for EO)

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9
Q

VGP Activation

A

Can be armed within 30 nm radial distance of destination
Activated when 5 nm from FAF or within 30 nm of destination and “activate vectors”
*Do NOT arm or activate VGP in a holding pattern

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10
Q

ILS “Checkpoints”

A

1500 RA – System attempts to arm the highest approach capability
800 RA – Approach capability locked in

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11
Q

Autothrottle Low Speed Protection

A

With flaps 0:
Below 20,000’ – 1.2 Vs
20,000’-30,000’ – Linear between 1.2 Vs and 1.02 LSA
Above 30,000’ – 1.02 LSA

Flaps not 0: 1.2 Vs

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12
Q

Autothrottle Disengagement

A

AT disengages when:

  • Touchdown
  • Thrust reverse during RTO
  • TLA > TOGA
  • Difference in TLA > 8 degrees
  • AT failure
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