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

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 _____

800 feet RA.

950 ft RA.

1 000 ft RA.

1 200 ft RA.

Correct! Wrong!

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

FMC

MCP

FCC

Correct! Wrong!

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

False.

True

Correct! Wrong!

It does!

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

Blank.

The aircraft's actual speed.

The FMC speed.

Correct! Wrong!

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

10 degrees or less

15 degrees or less.

5 degrees or less

6 degrees or less

Correct! Wrong!

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

True.

False.

Correct! Wrong!

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

False.

True.

Correct! Wrong!

Minimum speed reversion is NOT available in that case.

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.

10 seconds.

5 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.

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

FD roll commands hold current heading.

FD roll commands hold current ground track.

FD roll commands hold current heading until passing 400 ft.

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

Correct! Wrong!

The Roll Engaged Mode annunciation on the FMA is blank.

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:

600 fpm.

1200 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.

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

The aircraft will descend 500 feet to the new pressure level

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

The aircraft will climb 500 feet to the new pressure level

You cannot change the altitude when in ALT HOLD

Correct! Wrong!

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

VNAV.

VNAV PTH.

VNAV ALT.

VNAV SPD.

Correct! Wrong!

VNAV ALT maintains altitude.

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

One

Three

Fours (two for each channel)

Two

Correct! Wrong!

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

0.65 M

0.60 M

0.70 M

Correct! Wrong!

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

500 feet

800 feet

200 feet

2500 feet

Correct! Wrong!

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

False.

True.

Correct! Wrong!

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

IAS/MACH displays opens up and shows 250 kts.

IAS/MACH displays opens up and shows FMC target speed

IAS/MACH displays opens up and shows slashes.

IAS/MACH displays opens up and shows dashes.

Correct! Wrong!

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

The initial selected altitude is held.

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

Then V/S mode is automatically activated.

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 8 degrees of runway heading, 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.

Correct! Wrong!

LNAV guidance becomes active at 50 feet AGL

After a normal takeoff which pitch command can you expect?

V2 to V2+15kt

V2+20kt

V2 to V2+20kt

Correct! Wrong!

Antenna switching from tail antenna to nose antenna occurs when:

LOC frequency is selected only.

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

VOR frequency is selected only.

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

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.

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 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.

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.

Correct! Wrong!

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

V2+10.

V2 or airspeed at lift-off.

V2.

V2 + 20.

Correct! Wrong!

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

False.

True.

Correct! Wrong!

The Automatic Flight System (AFS) consists of:

The Autothrottles.

The autopilots.

All statements are correct.

The Flight Directors.

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!

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.

True.

False.

Correct! Wrong!

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

100 feet.

200 feet.

500 feet.

Correct! Wrong!

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.

20 feet.

100 feet.

50 feet.

Correct! Wrong!

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

MCP SPD

VNAV

CWS P

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 lift–off, the FD command bars automatically appear for both pilots.

2000 feet AGL.

1000 feet AGL.

1500 feet AGL.

2500 feet AGL.

Correct! Wrong!

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

10 degrees nose up and 60 kt IAS.

15 degrees nose up and 84 kt IAS.

15 degrees nose up and 60 kt IAS.

0 degrees nose up and 84 kt IAS.

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?

ARM - HDG SEL - TOGA

ARM - LNAV - FMC SPD

N1 - LNAV - MCP SPD

N1 - HDG SEL - VNAV

Correct! Wrong!

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!

The underspeed symbol in the MCP Speed window is a:

Steady 'A'.

Steady '8'.

Flashing 'A'.

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!

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

The stabilizer is out of trim.

Both autopilots have reverted to CWS mode.

A normal condition.

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 engages in full go-around mode.

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

The F/D command bars remain out of view.

Correct! Wrong!

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

False.

True.

Correct! Wrong!

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

LNAV disengages.

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

The autopilot disengages.

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.

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!

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

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

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

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 _____.

The second autopilot engagement.

1200 ft RA.

APP capture.

800 feet RA.

Correct! Wrong!

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?

GA - TOGA

MCP SPD - GA

N1 - VOR LOC - TOGA

GA - LNAV - MCP SPD

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.

Remains stationary.

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

Correct! Wrong!

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

3 NM.

1.5 NM

5 NM

2NM

Correct! Wrong!

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

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!

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 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!

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

Autothrottle computer.

FMC.

IRUs.

Correct! Wrong!

The AUTOLAND warning light flashed RED if:

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 feet

AP disengages and ILS deviation occurs below 200 feet

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

1/3

1/2 dot

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.

15 degrees

10 degrees

13 degrees

8 degrees

Correct! Wrong!

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

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, 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 at least and the associated sensors are operating normally for an automatic landing

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

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:

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

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.

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 and the STAB TRIM AUTOPILOT cutout switch is at NORMAL.

Correct! Wrong!

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

50 feet

35 feet

100 feet

27 feet

Correct! Wrong!

FLARE engaged is annunciated and FD command bars retract.

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

Display the Vref speed used during the final approach.

Display the flap manoeuvring speed.

Become blank.

Correct! Wrong!

With the AT Arm switch at ARM, the AT go–around mode is armed:

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.

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

Correct! Wrong!

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

The FMC is not providing autothrottle with N1 limit values.

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

The AT is using the upgraded BLT performance information.

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

Correct! Wrong!

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

400 ft RA.

250 ft RA.

500 ft RA.

350 feet RA.

Correct! Wrong!

If engaged the autothrottle will disengage ____ after landing touchdown.

2 seconds

5 seconds

7 seconds

6 seconds

Correct! Wrong!

Which Autothrottle modes permit manual thrust change without Autothrottle interference?

Only THR HLD

THR HLD and ARM

Correct! Wrong!

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

10–30 degrees selectable.

35 degrees.

40 degrees.

30 degrees.

Correct! Wrong!

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

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

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.

It is operational at all time.

Correct! Wrong!

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

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

800 feet RA.

400 feet RA.

200 ft RA.

500 ft RA.

Correct! Wrong!

The Flight Director Comparator monitors:

The IRS headings.

The symbol generators.

The command bar positions.

Correct! Wrong!

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.

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

True.

False

Correct! Wrong!

LNAV mode terminates whenever:

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

HDG SEL mode is engaged only.

Either HDG SEL, VOR or LOC mode is armed.

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 disengage but the aircraft will remain in approach logic

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

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

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

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.

Between 2 and 5 seconds depending on the altitude.

Immediately.

2 seconds.

4 seconds.

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.

+ 10 knots or - 5 knots

+ 5 knots or - 10 knots

+ or - 10 knots

+ 15 knots or -10 knots.

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 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 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 250 knots or less or after FD LOC capture in the APP mode.

Correct! Wrong!

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

Totally disengage.

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

Revert to CWS P and CWS R.

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.

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

True

False.

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.

False.

True

Correct! Wrong!

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

Boeing 737NG - Automatic Flight

Boeing 737NG – Automatic Flight

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 _____

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

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

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

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

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

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

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.

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

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:

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

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

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

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.

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

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

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

LNAV arming criteria on the ground:

After a normal takeoff which pitch command can you expect?

Antenna switching from tail antenna to nose antenna occurs when:

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:

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

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

The Automatic Flight System (AFS) consists of:

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:

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.

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

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.

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

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 lift–off, the FD command bars automatically appear for both pilots.

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

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?

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

The underspeed symbol in the MCP Speed window is a:

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

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

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 ?

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

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

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?

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

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 _____.

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?

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

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

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.

VNAV mode is terminated by any one of the following:

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

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

The AUTOLAND warning light flashed RED if:

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.

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.

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

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:

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

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

With the AT Arm switch at ARM, the AT go–around mode is armed:

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

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

If engaged the autothrottle will disengage ____ after landing touchdown.

Which Autothrottle modes permit manual thrust change without Autothrottle interference?

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

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

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

The Flight Director Comparator monitors:

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

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

LNAV mode terminates whenever:

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

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

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.

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.

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

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.

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

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

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