Boeing 737 MAX - Automatic Flight - SmartCockpit - Airline training guides, Aviation, Operations, Safety

Dual channel autopilot operation is possible only when two generators are powering the busses.

True.

False.

Correct! Wrong!

With VNAV engaged, the AFDS (Autopilot Flight Director System) pitch and AT modes are commanded by the:

MCP

FCC

FMC

Correct! Wrong!

If engaged the autothrottle will disengage ____ after landing touchdown.rn

7 seconds

2 seconds

6 seconds

5 seconds

Correct! Wrong!

One VHF NAV receiver must be tuned to an ILS frequency before the approach mode can be selected. For a dual AP approach, the second VHF NAV receiver must be tuned to the ILS frequency and the corresponding AP engaged in CMD prior to _____.

800 feet RA.

1200 ft RA.

The second autopilot engagement.

APP capture.

Correct! Wrong!

When control wheel pressure is released during CWS roll operation, the airplane will roll wings level when the bank angle is:

15 degrees or less.

10 degrees or less

6 degrees or less

5 degrees or less

Correct! Wrong!

The AT Disengage flashing light (amber) indicates an airspeed error under the following conditions: inflight, flaps not up and airspeed differs from commanded value by _______ and is not approaching commanded value. rn

+ 10 knots or - 5 knots

+ 5 knots or - 10 knots

+ or - 10 knots

+ 15 knots or -10 knots.

Correct! Wrong!

The Control wheel force required to override the Autopilot COMMAND mode is:

The same as normal CWS force.

Greater than normal CWS force

Less than normal CWS force

Correct! Wrong!

Localizer can be intercepted in HDG SEL, LNAV, or CWS R.

False.

True.

Correct! Wrong!

Which of the following occurs when a TOGA switch is pressed below 2000 feet RA for a flight director go-around from a single autopilot ILS approach?

The autothrottle advances thrust levers to reduced go-around N1.

All statements are correct.

The autopilot disengages.

GA mode of the flight director engages.

Correct! Wrong!

If the MCP selected Altitude is changed during ALT ACQ mode:

The pitch mode prior to ALT ACQ is automatically re-engaged.

Then V/S mode is automatically activated.

The initial selected altitude is held.

Correct! Wrong!

If an engine fails while the autothrottle is in N1 mode, the thrust lever of the failed engine:

Retracts a few degrees and returns to or above the other thrust lever position.

Advances a few degrees and returns to or below the other thrust lever position.

Remains stationary.

Correct! Wrong!

The Flight Director Comparator monitors:

The command bar positions.

The symbol generators.

The IRS headings.

Correct! Wrong!

The underspeed symbol in the MCP Speed window is a:

Steady 'A'.

Steady '8'.

Flashing 'A'.

Correct! Wrong!

The LOC capture point is variable and depends on intercept angle and rate of closure. Capture occurs no later than _____. Upon LOC capture, VOR LOC annunciates captured, SINGLE CH is annunciated for AP status, the previous roll mode disengages and the airplane turns to track the LOC.

1.5 dot

1/2 dot

1/3

Correct! Wrong!

The autopilot flare maneuver starts at approximately ____ feet RA and is completed at touchdown.rn

27 feet

100 feet

50 feet

35 feet

Correct! Wrong!

FLARE engaged is annunciated and FD command bars retract.

Moving the autopilot Stabilizer Trim Cutout Switch to the CUTOUT position will disengage the autopilot.

True.

False.

Correct! Wrong!

Which Autothrottle modes permit manual thrust change without Autothrottle interference?

Only THR HLD

THR HLD and ARM

Correct! Wrong!

The Autothrottle is engaged in FMC speed mode. What is displayed in the IAS/MACH display of the MCP?

The aircraft's actual speed.

The FMC speed.

Blank.

Correct! Wrong!

If windshear is encountered during FD takeoff or go-around, the FD pitch command bar provides commands to maintain V2+20 kts until vertical speed decreases to approximately:

1200 fpm.

600 fpm.

800 fpm.

1000 fpm.

Correct! Wrong!

As climb rate increases above approximately 600 fpm, the FD commands pitch attitudes which result in acceleration back to V2 + 20 kt.

VS mode automatically engages if ALT ACQ mode is engaged and a new MCP altitude is selected which is more than _____ different from previously selected altitude.

80 feet.

50 feet.

20 feet.

100 feet.

Correct! Wrong!

When in ALT HOLD at FL80 you change the barometric setting from STD to QNH 1030 (3041 In.Hg). What will the aircraft do?

You cannot change the altitude when in ALT HOLD

The aircraft will continue at FL80, but the ALT readout will change.

The aircraft will climb 500 feet to the new pressure level

The aircraft will descend 500 feet to the new pressure level

Correct! Wrong!

Two independent radio altimeters provide radio altitude to the respective FCCs. With a radio altimeter inoperative, the autopilot will disconnect ____ after LOC and GS capture.

2 seconds.

4 seconds.

Between 2 and 5 seconds depending on the altitude.rn

Immediately.

Correct! Wrong!

If thrust levers become separated more than 10 degrees during a dual channel approach (before FLARE armed is annunciated), the autothrottle is then disengaged.

False

True

Correct! Wrong!

This is true but after FLARE armed is annunciated

During takeoff with FD ON, the AFDS commands pitch attitude degrees after IAS.rn

15 degrees nose up and 60 kt IAS.

15 degrees nose up and 84 kt IAS.

0 degrees nose up and 84 kt IAS.

10 degrees nose up and 60 kt IAS.

Correct! Wrong!

LNAV arming criteria on the ground:

Origin runway in flight plan, active route entered in FMC, LNAV selected prior to TOGA.

Origin runway in flight plan, active route entered in FMC, track of first leg within 5 degrees of runway heading, LNAV selected prior to TOGA.

Origin runway in flight plan, active route entered in FMC, itrack of first leg within 7 degrees of runway track, LNAV selected prior to TOGA.

Origin runway in flight plan, active route entered in FMC, track of first leg within 8 degrees of runway heading, LNAV selected prior to TOGA.

Correct! Wrong!

LNAV guidance becomes active at 50 feet AGL

If the autopilot ALT HOLD mode is manually overriden with control column pressure, which of the following will occur?

The autopilot disengages.

LNAV disengages.

The autopilot changes to CWS P and returns to ALT HLD if control pressure released within 250 ft of selected altitude.

LEVEL CHANGE automatically engages.

Correct! Wrong!

If pitch is manually overridden while in ALT HOLD and control force is released within 250 feet of selected altitude, AP pitch mode engages in ALT ACQ and returns to selected altitude in ALT HOLD mode.

When a conflict occurs between the VNAV profile and the MCP altitude, the airplane levels and the pitch flight mode annunciation becomes:rn

VNAV SPD.

VNAV ALT.

VNAV.

VNAV PTH.

Correct! Wrong!

VNAV ALT maintains altitude.

The conditions for engaging the flight director in go-around mode are:

The F/D switches can be ON or OFF, inflight below 2,000 feet RA and not in takeoff mode, and the TO/GA switch pressed.

The F/D switches must be ON, inflight below 2,000 feet RA-and not in takeoff mode, and the TO/GA switch pressed.

The F/D switches must be ON, inflight below 800 feet RA-and not in take-off mode, and the TO/GA switch pressed.

Correct! Wrong!

What pitch mode is annunciated after takeoff when the autopilot is first engaged in CMD?

CWS P

VNAV

MCP SPD

Correct! Wrong!

What is the true statement about the Stabilizer Out Of Trim (STAB OUT OF TRIM) light?

Indicates that auto trim is degraded.

When no autopilot is engaged, it means that auto trim is inoperative. With autopilot engaged, it means that autopilot is not trimming stabilizer properly.

Operates only with autopilot engaged. Remains extinguished with autopilot not engaged.

It is operational at all time.

Correct! Wrong!

the illuminated (amber) light means that the autopilot is not trimming stabilizer properly.

After localizer or glideslope capture, during a single channel autopilot approach, CWS can be engaged by manually overriding pitch and or roll control forces.

False.

True.

Correct! Wrong!

After localizer or glideslope capture, during a single channel autopilot approach, CWS cannot be engaged by manually overriding pitch and/or roll control forces.

After a normal takeoff which pitch command can you expect? rn

V2 to V2+20kt

V2+20kt

V2 to V2+15kt rn

Correct! Wrong!

During a dual channel go-around, the MCP IAS/Mach display will:

Display the flap manoeuvring speed.

Become blank.

Display the Vref speed used during the final approach.

Correct! Wrong!

Normally, N1 limits and target N1 values are provided to the autothrottle by the:

Autothrottle computer.

IRUs.

FMC.

Correct! Wrong!

LNAV mode terminates whenever:

HDG SEL mode is engaged only.

Either HDG SEL, VOR or LOC mode is armed.

HDG SEL mode is engaged or upon VOR or LOC capture.

Correct! Wrong!

You are established on the ILS at 3000 ft and inadvertently press TOGA once. What will happen?

Nothing will happen since the aircraft has not descended below 2000 ft RA.

The AP will stay connected but the FMS will change to GA logic

The AP will disconnect and AT will add thrust to reduced G/A, FD will pitch 15 degrees nose up

The AP will disengage but the aircraft will remain in approach logic

Correct! Wrong!

Antenna switching from tail antenna to nose antenna occurs when:rnrn

LOC frequency is selected and VOR/LOC is armed or engaged.

VOR frequency is selected and VOR/LOC is armed or engaged.

VOR frequency is selected only.

LOC frequency is selected only.

Correct! Wrong!

When a localizer frequency is selected, VHF NAV radios automatically switch from tail antenna to nose antenna when VOR/LOC is annunciated (armed or engaged). If antenna switching does not occur, LOC mode is inhibited.

Dual channel AP operation is possible ONLY when two generators are powering the busses. rn

True.

False

Correct! Wrong!

When the pitch mode changes from VNAV SPD to ALT ACQ during an intermediate level off, the autothrottle will command a target IAS rather than Mach number.

False.

True.

Correct! Wrong!

Minimum speed reversion is also available when the Autothrottle is OFF and the AFDS is in ALT HOLD or after GS capture.rnrn

False.

True.

Correct! Wrong!

Minimum speed reversion is NOT available in that case.

What happens with the IAS/MACH display on the MCP if SPD INTV is pushed during VNAV operations?rn

IAS/MACH displays opens up and shows 250 kts.

IAS/MACH displays opens up and shows slashes.

IAS/MACH displays opens up and shows dashes.

IAS/MACH displays opens up and shows FMC target speed

Correct! Wrong!

Each autopilot can be engaged by pushing a separate CMD or CWS engage switch. Autopilot engagement in CMD or CWS is inhibited unless the below conditions are met:

No force is being applied to the control wheel and the STAB TRIM AUTOPILOT cutout switch is at NORMAL.

the STAB TRIM AUTOPILOT cutout switch is at NORMAL and one FD switch is ON.

No force is being applied to the control wheel and at least one autopilot channel is operational.

No force is being applied to the control wheel, at least one FD switch is ON, and the STAB TRIM AUTOPILOT cutout switch is at NORMAL.

Correct! Wrong!

VNAV mode is terminated by any one of the following:

Selecting another pitch mode, glideslope capture, reaching end of LNAV route, transition of glideslope intercept waypoint if GS is armed, crosstrack deviation exceeds twice the RNP

Selecting another pitch mode, glideslope capture, reaching end of LNAV route, transition of glideslope intercept waypoint if GS is armed, crosstrack deviation exceeds twice the RNP value during PTH descent for an active leg with a database vertical angle and LNAV not engaged.

Selecting another pitch mode, glideslope capture, transition of glideslope intercept waypoint if GS is armed, crosstrack deviation exceeds twice the RNP

Selecting another pitch mode, glideslope capture, reaching end of LNAV route, and transition of glideslope intercept waypoint if GS is armed

Correct! Wrong!

In the event of glideslope intercept waypoint transition, VNAV can be re-engaged.

if an engine failure occurs on the ground, the pitch command target speed at lift-off is _____, whichever is greater.

V2+10.

V2 + 20.

V2 or airspeed at lift-off.

V2.

Correct! Wrong!

After takeoff, the autopilot is engaged before flaps up. What is the correct mode (Thrust mode / Roll mode / Pitch mode) being displayed on the FMA? rnrn

ARM - LNAV - FMC SPD

N1 - LNAV - MCP SPD

N1 - HDG SEL - VNAV

ARM - HDG SEL - TOGA

Correct! Wrong!

When performing an autopilot ILS approach, the glide slope can be technically captured from above or below:

True.

False.

Correct! Wrong!

When flying on a geometrical path with VNAV engaged you push SPD INTV. What will happen? rn

VNAV PTH will remain engaged and MCP SPD will be annunciated in the FMA.

VNAV PTH will remain engaged and FMC SPD will be annunciated in the FMA.

VNAV SPD will engage and FMC SPD will be annunciated in the FMA.

VNAV SPD will engage and MCP SPD will be annunciated in the FMA.

Correct! Wrong!

During a reduced thrust takeoff, a second press of the TOGA switch below 800 feet above field elevation will change the thrust limit mode to GA and N1 reference bugs to increase to full GA thrust, thrust levers will not be in motion.

True.

False.

Correct! Wrong!

A second press of the TOGA switch above 800 feet above field elevation, thrust levers advance toward full GA thrust.

Bank angle is limited to 8 degrees below 400 feet, and _____ above 400 feet AGL.

40 degrees.

35 degrees.

30 degrees.

10u201330 degrees selectable.

Correct! Wrong!

With an active route entered in FMC, LNAV engages within _____ with any airplane heading.rn

1.5 NM

2NM

3 NM.

5 NM

Correct! Wrong!

Outside of 3 NM, airplane must be on intercept course of 90 degrees or less (intercept route segment before active waypoint).

For dual autopilot operation, both VHF NAV receivers must be tuned to the ILS frequency and both autopilots must be selected in CMD prior to _____

950 ft RA.

1 000 ft RA.

1 200 ft RA.

800 feet RA.

Correct! Wrong!

A mode change highlight symbol (rectangle) is drawn around each pitch, roll, autopilot status, and thrust engaged mode annunciation for a period of _____ after each engagement.

3 seconds.

2 seconds.

5 seconds.

10 seconds.

Correct! Wrong!

The mode change highlight symbol for CWS Mode annunciations (CWS R and CWS P) will flash for 10 seconds when CWS mode engages.

Above _____, selection of another pitch mode or engaging an autopilot will terminate the takeoff mode.

500 ft RA.

400 feet RA.

800 feet RA.

200 ft RA.

Correct! Wrong!

The FD can also be engaged in the takeoff mode with the FD switches off. If a TOGA switch is pushed after 80 knots below _____ and prior to 150 seconds after liftu2013off, the FD command bars automatically appear for both pilots.

1000 feet AGL.

1500 feet AGL.

2500 feet AGL.

2000 feet AGL.

Correct! Wrong!

During a single FD go-around, with a push of either TOGA switch:

FD roll commands hold current heading until passing 250 ft RA.

FD roll commands hold current ground track.

FD roll commands hold current heading.

FD roll commands hold current heading until passing 400 ft.

Correct! Wrong!

The Roll Engaged Mode annunciation on the FMA is blank.

As you push the TOGA switch for an automatic go-around, what is the correct FMA in terms of Thrust mode - Roll mode - Pitch mode?

N1 - VOR LOC - TOGA

MCP SPD - GA

GA - TOGA

GA - LNAV - MCP SPD

Correct! Wrong!

In the 'ARM' autothrottle mode, the thrust lever autothrottle servos maintain thrust at the selected N1 limit displayed on the thrust mode display.rn

True

False.

Correct! Wrong!

ARM mode = No autothrottle mode engaged. The thrust lever autothrottle servos are inhibited. The pilot can set thrust levers manually.

The AUTOLAND warning light flashed RED if:rn

AP disengages, stab trim or autothrottle warning occurs and ILS deviation occurs below 500 feet

AP disengages, stab trim warning occurs and ILS deviation occurs below 500 feet

AP disengages, stab trim warning occurs and ILS deviation occurs below 200 feetrn

AP disengages and ILS deviation occurs below 200 feet

Correct! Wrong!

When operating in 'ALT HOLD', the V/S mode is ARMED if the MCP altitude is changed by more than:

200 feet.

100 feet.

500 feet.

Correct! Wrong!

What is the minimum Mach number that can be selected in the IAS/MACH display of the MCP panel?

0.70 M

0.60 M

0.65 M

Correct! Wrong!

The AUTOLAND warning light is armed during dual ILS AP approach below ____ feet.

200 feet

500 feet

800 feet

2500 feet

Correct! Wrong!

With the AT Arm switch at ARM, the AT gou2013around mode is armed:

When descending below 2500 feet RA, when above 2000 feet RA with flaps not up or G/S captured, with the AFDS engaged.

When descending below 2000 feet RA, when above 2000 feet RA with flaps not up or G/S captured, with the AFDS engaged.

When descending below 2000 feet RA, when above 2000 feet RA with flaps not up or G/S captured, with or without the AFDS engaged.

When descending below 2000 feet RA, with G/S captured, with or without the AFDS engaged.

Correct! Wrong!

Maximum and minimum glideslope angles for autoland are 3.25 degrees and 2.5 degrees respectively.

False.

True

Correct! Wrong!

The following annunciation provide the flight crew with autoland system mode and status:

LAND 3 means two autopilots, three inertial sources at least and the associated sensors are operating normally for an automatic landing

LAND 3 means two autopilots, three inertial sources, the associated sensors are operating normally for an automatic landing and rollout and at least one FMS is operative.

LAND 3 means two autopilots, three inertial sources and the associated sensors are operating normally for an automatic landing and rollout.

LAND 3 means two autopilots, two inertial sources at least and the associated sensors are operating normally for an automatic landing

Correct! Wrong!

The Automatic Flight System (AFS) consists of:

All statements are correct.

The Autothrottles.

The Flight Directors.

The autopilots.

Correct! Wrong!

Automatic Flight Approach and Landing - If FLARE is not armed by approximately _____, both autopilots automatically disengage.

250 ft RA.

400 ft RA.

350 feet RA.

500 ft RA.

Correct! Wrong!

Pushing a CWS engage switch engages the autopilot pitch and roll axes in the CWS mode and displays CWS P and CWS R on the FMAs. The autopilot maneuvers the airplane in response to control pressures applied by either pilot. The control pressure is similar to that required for manual flight. If aileron pressure is released with 6 degrees or less bank, the autopilot rolls the wings level and holds existing heading. The heading hold feature with bank less than 6 degrees is inhibited when:

Below 2500 feet RA with the landing gear down or after FD VOR capture with TAS 200 knots or less or after FD LOC capture in the APP mode.

Below 1500 feet RA with the landing gear down or after FD VOR capture with TAS 200 knots or less or after FD LOC capture in the APP mode.

Below 2500 feet RA with the landing gear down or after FD VOR capture with TAS 250 knots or less or after FD LOC capture in the APP mode.

Below 1500 feet RA with the landing gear down or after FD VOR capture with TAS 250 knots or less or after FD LOC capture in the APP mode.

Correct! Wrong!

During a single engine FD go-around, the FD pitch commands ____ degrees nose up. As climb rate increases, FD pitch commands maintain a target speed.rn

8 degrees

10 degrees

15 degrees

13 degrees

Correct! Wrong!

The white AT LIM symbol appears on the upper display unit. What is the correct statement?

The N1 has been manually set and not by the FMC, therefore the AT LIM will be illuminated.

The autothrottle has reached the thrust limit for the selected assumed temperature.

The FMC is not providing autothrottle with N1 limit values.

The AT is using the upgraded BLT performance information.

Correct! Wrong!

The autopilot is engaged in ALT HOLD mode. The control column is then pushed, causing the autopilot to engage in CWS P mode. After the aircraft has descended 150 feet from the initial altitude the force applied to the control column is released and:

CWS P mode changes to ALT ACQ mode and the A/P remains atthe an altitude of 150 feet lower than the initial altitude and ALT HOLD engages.

CWS P mode changes to ALT ACQ mode and the A/P returns to the initial altitude and ALT HOLD engages.

CWS P remains engaged and the aircraft will maintain a constant pitch angle in the descent.

Correct! Wrong!

When one of the placard limit reversions (gear, flap or Vmo/Mmo) is reached, the overspeed limiting symbol appears in the MCP IAS Mach display.

False.

True.

Correct! Wrong!

The aircraft is climbing with the autopilot in CMD and the pilot pushes the control column forward. The autopilot will:

Revert to CWS P and the Roll axis remains in CMD.

Revert to CWS P and CWS R.

Totally disengage.

Correct! Wrong!

During a dual channel autopilot approach, the Autopilot Disengage light illuminates steady red when below 800 feet. What does this indicate?

A normal condition.

Both autopilots have reverted to CWS mode.

The stabilizer is out of trim.

Correct! Wrong!

Trimming the stabilizer with the electrical trim switch on the control wheel does not disengages the autopilot.rnrnrn

False.

True

Correct! Wrong!

It does!

How many independent Flight Control Computers (FCCs) are there in the AFDS?

Three

Fours (two for each channel)

One

Two

Correct! Wrong!

If the autopilot is engaged and either pilot's control wheel Trim Switch is activated:

The autopilot will disengage.

The stabiliser will move at a slow rate with the autopilot remains engaged.

The stabiliser will not move and the autopilot remains engaged.

Correct! Wrong!

A takeoff is commenced with both Flight Directors selected OFF. At 100 knots IAS a TOGA switch is pressed. What will happen to the F/D ?

The F/D command bars remain out of view.

The F/D command bars automatically appear for both pilots.

The F/D engages in full go-around mode.

Correct! Wrong!

During Autopilot CWS operation above 1500 feet RA, if the roll control force is released with less than 6 degrees of bank, the autopilot will:

Remain at the same bank angle.

Roll wings level and hold existing heading.

Roll wings level only.

Correct! Wrong!

Boeing 737 MAX - Automatic Flight

Boeing 737 MAX – Automatic Flight

Dual channel autopilot operation is possible only when two generators are powering the busses.

With VNAV engaged, the AFDS (Autopilot Flight Director System) pitch and AT modes are commanded by the:

If engaged the autothrottle will disengage ____ after landing touchdown.rn

One VHF NAV receiver must be tuned to an ILS frequency before the approach mode can be selected. For a dual AP approach, the second VHF NAV receiver must be tuned to the ILS frequency and the corresponding AP engaged in CMD prior to _____.

When control wheel pressure is released during CWS roll operation, the airplane will roll wings level when the bank angle is:

The AT Disengage flashing light (amber) indicates an airspeed error under the following conditions: inflight, flaps not up and airspeed differs from commanded value by _______ and is not approaching commanded value. rn

The Control wheel force required to override the Autopilot COMMAND mode is:

Localizer can be intercepted in HDG SEL, LNAV, or CWS R.

Which of the following occurs when a TOGA switch is pressed below 2000 feet RA for a flight director go-around from a single autopilot ILS approach?

If the MCP selected Altitude is changed during ALT ACQ mode:

If an engine fails while the autothrottle is in N1 mode, the thrust lever of the failed engine:

The Flight Director Comparator monitors:

The underspeed symbol in the MCP Speed window is a:

The LOC capture point is variable and depends on intercept angle and rate of closure. Capture occurs no later than _____. Upon LOC capture, VOR LOC annunciates captured, SINGLE CH is annunciated for AP status, the previous roll mode disengages and the airplane turns to track the LOC.

The autopilot flare maneuver starts at approximately ____ feet RA and is completed at touchdown.rn

Moving the autopilot Stabilizer Trim Cutout Switch to the CUTOUT position will disengage the autopilot.

Which Autothrottle modes permit manual thrust change without Autothrottle interference?

The Autothrottle is engaged in FMC speed mode. What is displayed in the IAS/MACH display of the MCP?

If windshear is encountered during FD takeoff or go-around, the FD pitch command bar provides commands to maintain V2+20 kts until vertical speed decreases to approximately:

VS mode automatically engages if ALT ACQ mode is engaged and a new MCP altitude is selected which is more than _____ different from previously selected altitude.

When in ALT HOLD at FL80 you change the barometric setting from STD to QNH 1030 (3041 In.Hg). What will the aircraft do?

Two independent radio altimeters provide radio altitude to the respective FCCs. With a radio altimeter inoperative, the autopilot will disconnect ____ after LOC and GS capture.

If thrust levers become separated more than 10 degrees during a dual channel approach (before FLARE armed is annunciated), the autothrottle is then disengaged.

During takeoff with FD ON, the AFDS commands pitch attitude ____ degrees after ____ IAS.rn

LNAV arming criteria on the ground:

If the autopilot ALT HOLD mode is manually overriden with control column pressure, which of the following will occur?

When a conflict occurs between the VNAV profile and the MCP altitude, the airplane levels and the pitch flight mode annunciation becomes:rn

The conditions for engaging the flight director in go-around mode are:

What pitch mode is annunciated after takeoff when the autopilot is first engaged in CMD?

What is the true statement about the Stabilizer Out Of Trim (STAB OUT OF TRIM) light?

After localizer or glideslope capture, during a single channel autopilot approach, CWS can be engaged by manually overriding pitch and or roll control forces.

After a normal takeoff which pitch command can you expect? rn

During a dual channel go-around, the MCP IAS/Mach display will:

Normally, N1 limits and target N1 values are provided to the autothrottle by the:

LNAV mode terminates whenever:

You are established on the ILS at 3000 ft and inadvertently press TOGA once. What will happen?

Antenna switching from tail antenna to nose antenna occurs when:rnrn

Dual channel AP operation is possible ONLY when two generators are powering the busses. rn

When the pitch mode changes from VNAV SPD to ALT ACQ during an intermediate level off, the autothrottle will command a target IAS rather than Mach number.

Minimum speed reversion is also available when the Autothrottle is OFF and the AFDS is in ALT HOLD or after GS capture.rnrn

What happens with the IAS/MACH display on the MCP if SPD INTV is pushed during VNAV operations?rn

Each autopilot can be engaged by pushing a separate CMD or CWS engage switch. Autopilot engagement in CMD or CWS is inhibited unless the below conditions are met:

VNAV mode is terminated by any one of the following:

if an engine failure occurs on the ground, the pitch command target speed at lift-off is _____, whichever is greater.

After takeoff, the autopilot is engaged before flaps up. What is the correct mode (Thrust mode / Roll mode / Pitch mode) being displayed on the FMA? rnrn

When performing an autopilot ILS approach, the glide slope can be technically captured from above or below:

When flying on a geometrical path with VNAV engaged you push SPD INTV. What will happen? rn

During a reduced thrust takeoff, a second press of the TOGA switch below 800 feet above field elevation will change the thrust limit mode to GA and N1 reference bugs to increase to full GA thrust, thrust levers will not be in motion.

Bank angle is limited to 8 degrees below 400 feet, and _____ above 400 feet AGL.

With an active route entered in FMC, LNAV engages within _____ with any airplane heading.rn

For dual autopilot operation, both VHF NAV receivers must be tuned to the ILS frequency and both autopilots must be selected in CMD prior to _____

A mode change highlight symbol (rectangle) is drawn around each pitch, roll, autopilot status, and thrust engaged mode annunciation for a period of _____ after each engagement.

Above _____, selection of another pitch mode or engaging an autopilot will terminate the takeoff mode.

The FD can also be engaged in the takeoff mode with the FD switches off. If a TOGA switch is pushed after 80 knots below _____ and prior to 150 seconds after liftu2013off, the FD command bars automatically appear for both pilots.

During a single FD go-around, with a push of either TOGA switch:

As you push the TOGA switch for an automatic go-around, what is the correct FMA in terms of Thrust mode - Roll mode - Pitch mode?

In the 'ARM' autothrottle mode, the thrust lever autothrottle servos maintain thrust at the selected N1 limit displayed on the thrust mode display.rn

The AUTOLAND warning light flashed RED if:rn

When operating in 'ALT HOLD', the V/S mode is ARMED if the MCP altitude is changed by more than:

What is the minimum Mach number that can be selected in the IAS/MACH display of the MCP panel?

The AUTOLAND warning light is armed during dual ILS AP approach below ____ feet.

With the AT Arm switch at ARM, the AT gou2013around mode is armed:

Maximum and minimum glideslope angles for autoland are 3.25 degrees and 2.5 degrees respectively.

The following annunciation provide the flight crew with autoland system mode and status:

The Automatic Flight System (AFS) consists of:

Automatic Flight Approach and Landing - If FLARE is not armed by approximately _____, both autopilots automatically disengage.

During a single engine FD go-around, the FD pitch commands ____ degrees nose up. As climb rate increases, FD pitch commands maintain a target speed.rn

The white AT LIM symbol appears on the upper display unit. What is the correct statement?

The autopilot is engaged in ALT HOLD mode. The control column is then pushed, causing the autopilot to engage in CWS P mode. After the aircraft has descended 150 feet from the initial altitude the force applied to the control column is released and:

When one of the placard limit reversions (gear, flap or Vmo/Mmo) is reached, the overspeed limiting symbol appears in the MCP IAS Mach display.

The aircraft is climbing with the autopilot in CMD and the pilot pushes the control column forward. The autopilot will:

During a dual channel autopilot approach, the Autopilot Disengage light illuminates steady red when below 800 feet. What does this indicate?

Trimming the stabilizer with the electrical trim switch on the control wheel does not disengages the autopilot.rnrnrn

How many independent Flight Control Computers (FCCs) are there in the AFDS?

If the autopilot is engaged and either pilot's control wheel Trim Switch is activated:

A takeoff is commenced with both Flight Directors selected OFF. At 100 knots IAS a TOGA switch is pressed. What will happen to the F/D ?

During Autopilot CWS operation above 1500 feet RA, if the roll control force is released with less than 6 degrees of bank, the autopilot will:

During takeoff with FD ON, the AFDS commands pitch attitude degrees after IAS.rn