Autoflight Flashcards

1
Q

(All) Which roll modes are affected by the Bank Angle Select Knob?

A
  • Bank Angle Select Knob sleeve provides selection of bank limits for HDG HLD, HDG SEL, and VOR.
  • AOB limiting is inhibited in LOC CAP & FMS NAV modes.

Note: During FMS NAV mode operations, AOB limit is 15° if NAV is engaged, slats are extended and airspeed < AFMC computed minimum speed.

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2
Q

When do auto throttles engage in Clamp (CLMP) Mode?

A
  • Aircraft is on the ground for > 20 sec with autothrottle in EPR mode and airspeed > 60 KIAS.
  • If IAS or MACH mode is selected while in flight with auto throttles engaged in VERT SPD, ALT HOLD, SPD SEL or MACH SEL modes.
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3
Q

(88, 90) In IAS/MACH mode, how are pitch changes related to throttle movement?

A

IAS or Mach mode is engaged by pushing IAS MACH button.
• PFD displays FD commands to maintain selected Mach or indicated airspeed and AP (if engaged) will adjust pitch attitude to maintain selected speed.

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4
Q

(88, 90) Function of the IAS MACH Pitch Mode Select Button:

A
  • Selects existing IAS (below 27,000feet) or Mach (above 27,000 feet and above .5 Mach) for DFGS pitch mode.
  • Using pitch to control speed is indicated by an “S” (airspeed) or “M” (Mach) symbol and desired airspeed or Mach respectively.
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5
Q

(88, 90) In VERT SPD and ALT HLD modes, how is airspeed controlled?

A
  • Airspeed is controlled by autothrottles which are programmed by SPD/MACH select knob.
  • SPD SEL or MACH SEL can be engaged during any phase of flight except when TO, GA or TO FLX is selected on TRP or retard mode is engaged.
    • With autothrottle in SPD SEL or MACH SEL mode, auto-throttles seek and maintain reference Speed/Mach selected in SPD/MACH window except when Alpha speed reference is higher.
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6
Q

(All) What are the indications when autothrottles are disconnected?

A
  • THROTTLE Warning Light (red) flashes
  • Pushing autothrottle disconnect button on either throttle or re-selecting AUTO THROT switch to AUTO THROT position extinguishes light.
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7
Q

(88, 90) What are the conditions and indications when the autopilot is disconnected?

A

The AP is disengaged and the red AP warning light on FMA flashes in the following conditions:
• AP switch is off
• AP malfunction is detected
• DFGC switch is moved from selected position
• AUTOPILOT REL button on either control wheel is pushed
• Primary horizontal stabilizer trim is manually operated
• Activation of the stick pusher.

NOTES

  • In addition, flashing AP light is accompanied by aural and vocal warnings in all AP disengagements.
  • Loss of electrical power will also disengage the autopilot, however, with NO warning light and NO vocal warning
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8
Q

(88, 90) What is the meaning of ALFA SPD annunciation in the throttle window of the FMA?

A
  • Alpha speed is a safe margin above stall speed.
  • Throttles are controlled to seek and maintain Alpha speed reference indicated by the Fast/Slow display on the PFD
  • ALFA SPD mode is engaged automatically when autothrottle is in SPD SEL or MACH SEL mode and selected SPD/MACH value is less than safe minimum airspeed for existing slat/flap configuration.
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9
Q

(88, 90) Describe Flight Mode Annunciator (FMA) windows:

A

The four FMA windows are (from left to right):
• FMA Thrust Window (green) Displays existing autothrottle mode.
• FMA Arm Window (amber) Displays armed mode for roll or pitch.
• FMA Roll Window (green) Displays existing roll mode.
• FMA Pitch Window (green) Displays existing pitch mode.

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10
Q

(88, 90) Explain how AUTOLAND mode of the auto flight system may be disarmed after autoland has been armed and both the localizer and glideslope are in the track mode:

A

Once the autoland has been armed and both the localizer and glideslope are in the track mode (LND, LOC/TRK, GS/TRK) the autoland may be disengaged by accomplishing any of the following:
• Disengage the autopilot
• Push the TOGA button(s)
• Detune the ILS frequency

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11
Q

(88, 90) Explain the pitch and roll commands given by flight director when TOGA is selected (during takeoff)

A

Pitch Commands During takeoff
• Command bar on PFD commands pitch attitude to maintain V2+10 for 2-engine operation.

Engine failure - pitch commands for one engine operation:
• If airspeed ≥ V2, command bar commands pitch att. to maintain V2.
• If airspeed is between V2 and V2+10, command bar commands pitch att. to maintain existing airspeed.
• If airspeed ≥ V2+10, command bar commands a pitch attitude to maintain V2+10.

Roll commands: After lift-off, roll command bar will command wings level to maintain heading.

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12
Q

(88, 90) Explain the pitch and roll commands given by the flight director when TOGA is selected during go around.

A

Pitch commands in go-around mode
• Command bar commands a pitch attitude to maintain DFGC computed go-around speed
- Airspeed at TOGA switch activation, but
- NLT 1.3 Vs + 5 or no greater than 1.3 Vs + 25 of the landing flap configuration)

Roll Commands
• During go-around: Existing magnetic heading maintained and roll command bar commands wing level.

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13
Q

(88, 90) Understand the FMA annunciation CLMP and when it is displayed:

A

CLMP (Controls Locked Manual Power):
• ATS in CLMP mode.
• Power is removed from ATS servo (throttles remain stationary).
• In flight: Results from selecting IAS/MACH on FGCP.
• On ground: Airplane is on the ground > 20 sec with autothrottle in EPR mode and airspeed > 60 kts

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14
Q

(88, 90) Understand the FMA annunciation FMS SPD and when it is displayed:

A

• FMS SPD – (FMS VNAV mode engaged.) Throttles being controlled by FMS to maintain speed.

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15
Q

(88, 90) Meaning of FMA annunciation FMS EPR and when it is displayed:

A

• FMS EPR – (FMS VNAV mode engaged.) Throttles being controlled by FMS to maintain EPR.

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16
Q

(88, 90) What happens when HDG select knob is pushed in fully?

A

Pushed to Full Detent
• Engages heading hold mode.
• AP/FD either maintains existing heading - or-
• If AOB > 3°, rolls airplane wings level and maintains that heading.

17
Q

(88, 90) What happens when HDG select knob is pushed to the first detent only?

A

Pushed to First Detent

• Provides fast rate of heading adjustment.

18
Q

(88, 90) What happens when adjusting vertical speed during altitude capture? Other modes this applies to?

A
  • Vertical speed rate adjustments during/after altitude capture disengages altitude capture mode
  • Pitch control reverts to vertical speed mode.
  • True for ALT CAP, ALT HLD, or VNAV modes
19
Q

(88, 90) When can SPD SEL (Speed Select) Mode be engaged?

A

SPD SEL can be engaged in any phase of flt except when
• TO, GA or TO FLX is selected on TRP - or -
• Retard mode is engaged.

20
Q

(88, 90) When will autopilot/flight director revert to vertical speed if engaged in SPD SEL (Speed Select) mode:

A

If autopilot/FD is already engaged in IAS or MACH mode

Engagement of auto throttle in SPD SEL or MACH SEL will cause AP/FD to revert to vertical speed mode at existing vertical speed. VERT SPD annunciation will flash for 5 seconds on the FMA.

Note: Pitch Profile Readout/window on FGCP will display/ capture existing vertical speed when SPD SEL is pressed.