Automatic Flight B737NG

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Pregunta 1 de 62
1. Pregunta
If during a climb with autopilot engaged, the ALT HOLD switch is pressed, the aircraft will
Stop the climb and level off.
Correcto Incorrecto Correct answer

Continue the climb to the next 1000 feet level and level off.
Correcto Incorrecto Correct answer

Continue the climb to the preset altitude selected, as the altitude acquire mode is now armed.
Correcto Incorrecto Correct answer

Correcto
Incorrecto
Pregunta 2 de 62
2. Pregunta
The underspeed symbol in the MCP Speed window is a
Steady "A".
Correcto Incorrecto Correct answer

Flashing "8".
Correcto Incorrecto Correct answer

Flashing "A".
Correcto Incorrecto Correct answer

Correcto
Incorrecto

Pregunta 3 de 62

3. Pregunta

The autopilot is engaged in ALT HOLD mode. The controlcolumn 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.

Correcto Incorrecto Correct answer

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

Correcto Incorrecto Correct answer

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.

Correcto Incorrecto Correct answer

Correcto

Incorrecto

Pregunta 4 de 62
4. Pregunta
The Automatic Flight System (AFS) provides speed, pitch and thrust commands to avoid exceeding the following limit speeds
Vmo / Mmo. Wing flap placard. Turbulence penetration. Minimum speed (maximum angle of attack).
Correcto Incorrecto Correct answer

Vmo / Mmo. Minimum speed (maximum angle of attack).
Correcto Incorrecto Correct answer

Vmo / Mmo. Wing flap placard. Landing gear placards. Minimum speed (maximum angle of attack).
Correcto Incorrecto Correct answer

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Pregunta 5 de 62
5. Pregunta
With autopilot A engaged, the altitude selected on the MCP is referenced to
The standby altimeter.
Correcto Incorrecto Correct answer

The First Officer's altimeter.
Correcto Incorrecto Correct answer

The Captain's altimeter.
Correcto Incorrecto Correct answer

Correcto
Incorrecto
Pregunta 6 de 62
6. Pregunta
During a dual channel autopilot approach, the Autopilot Disengage light illuminates steady red when below 800 feet. This indicates
A normal condition
Correcto Incorrecto Correct answer

The stabilizer is out of trim.
Correcto Incorrecto Correct answer

Both autopilots have reverted to CWS mode.
Correcto Incorrecto Correct answer

Correcto
Incorrecto
Pregunta 7 de 62
7. Pregunta
During a VNAV PATH descent, VNAV remains engaged until
Glideslope capture, or Another pitch mode is selected, or Flaps are extended beyond 15, or LNAV is disengaged without localiser capture.
Correcto Incorrecto Correct answer

Glideslope capture, or Another pitch mode is selected, or Flaps are extended beyond 25, or LNAV is disengaged without localiser capture.
Correcto Incorrecto Correct answer

Approach mode is armed, or Another pitch mode is selected, or Flaps are extended beyond 25, or LNAV is disengaged without localiser capture.
Correcto Incorrecto Correct answer

Correcto
Incorrecto
Pregunta 8 de 62
8. Pregunta
Which radio altimeter provides radio altitude to the autothrottle
Both the Captain's and the First Officer's.
Correcto Incorrecto Correct answer

The First Officer's.
Correcto Incorrecto Correct answer

The Captain's.
Correcto Incorrecto Correct answer

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Pregunta 9 de 62
9. Pregunta
VNAV climbs and descents are
Constrained by the selected cabin altitude.
Correcto Incorrecto Correct answer

Not constrained by the selected MCP altitude.
Correcto Incorrecto Correct answer

Constrained by the selected MCP altitude.
Correcto Incorrecto Correct answer

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Pregunta 10 de 62
10. Pregunta
During an autopilot go-around, the Autopilot Disengage light illuminates steady red. This indicates
The altitude acquire mode is inhibited (Stabilizer not trimmed for single A/P operation).
Correcto Incorrecto Correct answer

One or more autopilots have reverted to CWS mode.
Correcto Incorrecto Correct answer

A normal condition.
Correcto Incorrecto Correct answer

Correcto
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Pregunta 11 de 62
11. Pregunta
If VOR/LOC mode is fully engaged during an ILS approach and then the master VHF NAV receiver is placed in the AUTO tuning mode
The VOR/LOC mode automatically disengages.
Correcto Incorrecto Correct answer

The go-around is initiated automatically without pressing either TOGA switch.
Correcto Incorrecto Correct answer

The VOR/LOC mode remains engaged.
Correcto Incorrecto Correct answer

Correcto
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Pregunta 12 de 62
12. Pregunta
Dual channel Autopilot operation is possible
Without any generator busses being energised.
Correcto Incorrecto Correct answer

When AC power is available to at least one generator bus.
Correcto Incorrecto Correct answer

Only when two generators are powering the busses.
Correcto Incorrecto Correct answer

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Pregunta 13 de 62
13. Pregunta
When intercepting the ILS with APP mode armed
On all airplanes, localizer must be captured prior to glideslope.
Correcto Incorrecto Correct answer

The second autopilot can be engaged.
Correcto Incorrecto Correct answer

On some airplanes, glideslope may be captured prior to localizer.
Correcto Incorrecto Correct answer

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Pregunta 14 de 62
14. Pregunta
If the autothrottle is engaged and an autothrottle disengage switch is pressed
The autothrottle disengages.The A/T disengage lightsflash and the A/T ARM switch trips OFF. A second press and the A/T disengage lights extinguish.
Correcto Incorrecto Correct answer

The autothrottle disengages.The A/T disengage lightsflash, the A/T disengage warning tone sounds and the A/T ARM switch trips OFF. A second press and the A/T disengage lights extinguish and the warning tone.
Correcto Incorrecto Correct answer

The autothrottle disengages provided the button is held formore than two seconds. The A/T disengage lights flash and the A/T ARM switch trips OFF. A second press and the A/T disengage lights extinguish.
Correcto Incorrecto Correct answer

Correcto
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Pregunta 15 de 62
15. Pregunta
Dual autopilot engagement is possible
Provided that both NAV receivers are tuned to the ILS frequency, APP mode is selected and the aircraft is above 800 feet RA.
Correcto Incorrecto Correct answer

At any time below 1500 feet RA.
Correcto Incorrecto Correct answer

Provided that both NAV receivers are tuned to the ILS frequency, VOR/LOC mode is selected and the aircraft is above 800 feet RA.
Correcto Incorrecto Correct answer

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Pregunta 16 de 62
16. Pregunta
The Autothrottle sets take-off thrust prior to
60 knots IAS during the take-off roll.
Correcto Incorrecto Correct answer

64 knots groundspeed during the take-off roll.
Correcto Incorrecto Correct answer

60 knots groundspeed during the take-off roll.
Correcto Incorrecto Correct answer

Correcto
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Pregunta 17 de 62
17. Pregunta
The bank angle limit selector sets the limit of bank angle when using
LNAV and heading select modes.
Correcto Incorrecto Correct answer

Heading select and VOR modes.
Correcto Incorrecto Correct answer

All roll modes.
Correcto Incorrecto Correct answer

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Pregunta 18 de 62
18. Pregunta
What is the minimum Mach number that can be selected in the IAS/MACH display of the MCP panel
0.40 M
Correcto Incorrecto Correct answer

0.50 M
Correcto Incorrecto Correct answer

0.60 M
Correcto Incorrecto Correct answer

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Pregunta 19 de 62
19. Pregunta
After LOC and G/S are both captured, the APP mode can be exited by
Pressing the APP mode switch.
Correcto Incorrecto Correct answer

Disengaging the autopilot only.
Correcto Incorrecto Correct answer

Pressing a TOGA switch.
Correcto Incorrecto Correct answer

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Pregunta 20 de 62
20. Pregunta
During a single Autopilot approach, a Go-around is initiated by pressing a TOGA button. This causes
The autopilot to disengage.
Correcto Incorrecto Correct answer

The autothrottle to disengage.
Correcto Incorrecto Correct answer

The autopilot to remain engaged throughout the go-around.
Correcto Incorrecto Correct answer

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Pregunta 21 de 62
21. Pregunta
During a dual channel approach the second autopilot must be engaged in CMD by
500 feet radio altitude
Correcto Incorrecto Correct answer

800 feet radio altitude.
Correcto Incorrecto Correct answer

1500 feet radio altitude.
Correcto Incorrecto Correct answer

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Pregunta 22 de 62
22. Pregunta
The IAS/MACH display change over switch on the MCP panel will change the display between IAS and MACH when pressed. An automatic change over
Occurs at approximately FL350.
Correcto Incorrecto Correct answer

Does not occur.
Correcto Incorrecto Correct answer

Occurs at approximately FL260.
Correcto Incorrecto Correct answer

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Pregunta 23 de 62
23. Pregunta
During a Dual Channel Autoland Approach, the autopilots were disengaged at 200 feet RA and
Aft control column force may be required to hold the desired pitch attitude.
Correcto Incorrecto Correct answer

No additional control column force would be required to hold the desired pitch attitude.
Correcto Incorrecto Correct answer

Forward control column force may be required to hold the desired pitch attitude.
Correcto Incorrecto Correct answer

Correcto
Incorrecto
Pregunta 24 de 62
24. Pregunta
LNAV capture criteria is satisfied when
The aircraft is within 5 nm of the active route segmentirrespective of heading, orThe aircraft is greater than 5 nm. from the active route segment but the heading is on a intercept course of 90degrees or less and will intercept the route segment before the active waypoint.
Correcto Incorrecto Correct answer

The aircraft is greater than 5 nm from the active route segment but the heading is on a intercept course of 60 degrees or less and will intercept the route segment before the active waypoint.
Correcto Incorrecto Correct answer

The aircraft is within 3 nm of the active route segmentirrespective of heading, or The aircraft is greater than 3 nm from the active route segment but the heading is on a intercept course of 90 degrees or less and will intercept the route segment before the active waypoint.
Correcto Incorrecto Correct answer

Correcto
Incorrecto
Pregunta 25 de 62
25. Pregunta
If FLARE arm is not annunciated by approximately 350 feet radio altitude
Reselect APP mode on the MCP.
Correcto Incorrecto Correct answer

The second engaged autopilot will disengage automatically.
Correcto Incorrecto Correct answer

Both autopilots will disconnect automatically.
Correcto Incorrecto Correct answer

Correcto
Incorrecto
Pregunta 26 de 62
26. Pregunta
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
Roll wings level and hold existing heading.
Correcto Incorrecto Correct answer

Remain at the same bank angle.
Correcto Incorrecto Correct answer

Roll wings level only.
Correcto Incorrecto Correct answer

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Pregunta 27 de 62
27. Pregunta
If the Autothrottle is engaged during a touchdown
It will automatically disengage approximately 2 seconds after touchdown.
Correcto Incorrecto Correct answer

It will not automatically disengage after touchdown and should be manually disengaged.
Correcto Incorrecto Correct answer

It will automatically disengage approximately 5 seconds after touchdown.
Correcto Incorrecto Correct answer

Correcto
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Pregunta 28 de 62
28. Pregunta
The Autothrottle is engaged in FMC speed mode. What is displayed in the IAS/MACH display of the MCP
The FMC demanded speed.
Correcto Incorrecto Correct answer

Blank.
Correcto Incorrecto Correct answer

The aircraft's actual speed.
Correcto Incorrecto Correct answer

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Pregunta 29 de 62
29. Pregunta
During a dual channel approach, the autothrottle begins retarding the thrust at approximately
27 feet radio altitude.
Correcto Incorrecto Correct answer

50 feet radio altitude.
Correcto Incorrecto Correct answer

10 feet radio altitude.
Correcto Incorrecto Correct answer

Correcto
Incorrecto
Pregunta 30 de 62
30. Pregunta
The mode selector switches on the MCP panel will illuminate the letters ON to indicate that
The mode can be deactivated by selecting either F/D switch to OFF.
Correcto Incorrecto Correct answer

The mode can not be deactivated by pressing the mode switch a second time.
Correcto Incorrecto Correct answer

The mode can be deactivated by pressing the mode switch a second time.
Correcto Incorrecto Correct answer

Correcto
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Pregunta 31 de 62
31. Pregunta
During a Dual Channel Autoland, the autopilots
Must be manually disengaged after touchdown. The landing roll-out is executed manually after disengaging the A/P.
Correcto Incorrecto Correct answer

Must not be disengaged after touchdown until the airspeed is less than 60 knots.
Correcto Incorrecto Correct answer

May be manually disengaged after touchdown. The landing roll-out can be executed automatically.
Correcto Incorrecto Correct answer

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Pregunta 32 de 62
32. Pregunta
When operating in «ALT HOLD», the V/S mode is ARMED if the MCP altitude is changed by more than
500 feet.
Correcto Incorrecto Correct answer

200 feet.
Correcto Incorrecto Correct answer

100 feet.
Correcto Incorrecto Correct answer

Correcto
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Pregunta 33 de 62
33. Pregunta
During a dual channel go-around, the MCP IAS/Mach display will
Display the Vref speed used during the final approach.
Correcto Incorrecto Correct answer

Display the flap manoeuvring speed.
Correcto Incorrecto Correct answer

Become blank.
Correcto Incorrecto Correct answer

Correcto
Incorrecto
Pregunta 34 de 62
34. Pregunta
If the MCP selected Altitude is changed during ALT ACQ mode
The pitch mode prior to ALT ACQ is automatically re-engaged.
Correcto Incorrecto Correct answer

The initial selected altitude is held.
Correcto Incorrecto Correct answer

Then V/S mode is automatically activated.
Correcto Incorrecto Correct answer

Correcto
Incorrecto
Pregunta 35 de 62
35. Pregunta
The A/P go-around mode requires dual A/P operation and becomes armed when
A flap setting of 15 or more is selected.
Correcto Incorrecto Correct answer

LOC and GS capture is annunciated.
Correcto Incorrecto Correct answer

FLARE armed is annunciated.
Correcto Incorrecto Correct answer

Correcto
Incorrecto
Pregunta 36 de 62
36. Pregunta
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.
Correcto Incorrecto Correct answer

Totally disengage.
Correcto Incorrecto Correct answer

Revert to CWS P and CWS R.
Correcto Incorrecto Correct answer

Correcto
Incorrecto
Pregunta 37 de 62
37. Pregunta
Flight Director roll commands, from take-off mode engagement through to the take-off climbout, are
To maintain the heading selected in the heading window.
Correcto Incorrecto Correct answer

To hold the wings level.
Correcto Incorrecto Correct answer

To maintain the runway track.
Correcto Incorrecto Correct answer

Correcto
Incorrecto
Pregunta 38 de 62
38. Pregunta
LNAV mode terminates whenever
Either HDG SEL, VOR or LOC mode is armed.
Correcto Incorrecto Correct answer

HDG SEL mode is engaged only.
Correcto Incorrecto Correct answer

HDG SEL mode is engaged or upon VOR or LOC capture.
Correcto Incorrecto Correct answer

Correcto
Incorrecto
Pregunta 39 de 62
39. Pregunta
Upon Go-Around engagement during a fully automatic approach the autothrottles will
Advance the thrust levers toward the reduced go-around N1.
Correcto Incorrecto Correct answer

Advance the thrust levers toward the maximum go around N1.
Correcto Incorrecto Correct answer

Disengage.
Correcto Incorrecto Correct answer

Correcto
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Pregunta 40 de 62
40. Pregunta
During a single engine F/D go-around
The autothrottle will disengage.
Correcto Incorrecto Correct answer

The autothrottle will increase thrust to the reduced thrust go-around thrust setting.
Correcto Incorrecto Correct answer

The autothrottle will increase thrust to the full N1 limit.
Correcto Incorrecto Correct answer

Correcto
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Pregunta 41 de 62
41. Pregunta
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 take-off mode, and the TO/GA switch pressed.
Correcto Incorrecto Correct answer

The F/D switches must be ON, inflight below 2,000 feet RA-and not in take-off mode, and the TO/GA switch pressed.
Correcto Incorrecto Correct answer

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

Correcto
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Pregunta 42 de 62
42. Pregunta
A rectangle is drawn around each pitch, roll, CWS and thrust engaged mode annunciation (EFIS Flight Mode Annunciations) whenever
A mode change occurs from active to armed, and the rectangle remains for 10 seconds.
Correcto Incorrecto Correct answer

A mode change has occurred and the rectangle remains for 1 second.
Correcto Incorrecto Correct answer

A mode change has occurred and the rectangle remains for 10 seconds.
Correcto Incorrecto Correct answer

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Pregunta 43 de 62
43. Pregunta
During an ILS approach with both flight directors ON
The F/D command bars retract from view at approximately 50 feet RA.
Correcto Incorrecto Correct answer

The F/D command bars retract from view at approximately 200 feet RA.
Correcto Incorrecto Correct answer

The F/D command bars remain in view until after touchdown, giving full landing flare capability.
Correcto Incorrecto Correct answer

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Pregunta 44 de 62
44. Pregunta
The Flight Director Comparator monitors
The IRS headings.
Correcto Incorrecto Correct answer

The symbol generators.
Correcto Incorrecto Correct answer

The command bar positions.
Correcto Incorrecto Correct answer

Correcto
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Pregunta 45 de 62
45. Pregunta
An A/T LIM light when illuminated, or an A/T LIM annunciation (as installed) indicates
The autothrottle computer is calculating an FMC N1 limit for the affected engine or engines.
Correcto Incorrecto Correct answer

The autothrottle computer is calculating a degraded N1 limit for the affected engine or engines.
Correcto Incorrecto Correct answer

The autothrottles are positioned at their normal operating limit as calculated by the FMC.
Correcto Incorrecto Correct answer

Correcto
Incorrecto
Pregunta 46 de 62
46. Pregunta
Both MA lights on the MCP panel are illuminated during an approach indicating
Independent Flight Director operation.
Correcto Incorrecto Correct answer

Go-around mode is armed.
Correcto Incorrecto Correct answer

A Flight Director malfunction.
Correcto Incorrecto Correct answer

Correcto
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Pregunta 47 de 62
47. Pregunta
The STAB OUT OF TRIM light operates
Only when the autopilot is engaged.
Correcto Incorrecto Correct answer

At any time.
Correcto Incorrecto Correct answer

Only when the speed trim system is activated.
Correcto Incorrecto Correct answer

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Pregunta 48 de 62
48. Pregunta
The Altitude Alerting system is inhibited whenever
The wing flaps are extended past 25 or while the glideslope is captured.
Correcto Incorrecto Correct answer

The glideslope is captured.
Correcto Incorrecto Correct answer

The wing flaps are extended past 15 or while the glideslope is captured.
Correcto Incorrecto Correct answer

Correcto
Incorrecto
Pregunta 49 de 62
49. Pregunta
All AFDS modes can be disengaged by selecting another command mode or
By disengaging the A/P only.
Correcto Incorrecto Correct answer

By disengaging the A/P and turning the F/Ds off.
Correcto Incorrecto Correct answer

By turning the F/Ds off with the autopilot engaged.
Correcto Incorrecto Correct answer

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Pregunta 50 de 62
50. Pregunta
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.
Correcto Incorrecto Correct answer

The F/D command bars remain out of view.
Correcto Incorrecto Correct answer

The F/D command bars automatically appear for both pilots.
Correcto Incorrecto Correct answer

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Pregunta 51 de 62
51. Pregunta
If the autopilot disengage light is flashing amber, this indicates that
The light test switch is being held in position 2.
Correcto Incorrecto Correct answer

The autopilot has reverted to CMD pitch or roll while in CWS.
Correcto Incorrecto Correct answer

The autopilot has reverted to CWS pitch or roll while in CMD.
Correcto Incorrecto Correct answer

Correcto
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Pregunta 52 de 62
52. Pregunta
If an engine fails while the autothrottle is in N1 mode, the thrust lever of the failed engine
Remains stationary.
Correcto Incorrecto Correct answer

Retracts a few degrees and returns to or above the other thrust lever position.
Correcto Incorrecto Correct answer

Advances a few degrees and returns to or below the other thrust lever position.
Correcto Incorrecto Correct answer

Correcto
Incorrecto
Pregunta 53 de 62
53. Pregunta
What criteria must be met before autopilot engagement
No force is applied to the control wheel or column and the Stabiliser Trim Auto Pilot Cut-Out Switch is at NORMAL.
Correcto Incorrecto Correct answer

The Stabiliser Trim Auto Pilot Cut-Out Switch is at NORMAL only.
Correcto Incorrecto Correct answer

No force is applied to the control wheel or column, the Stabiliser Trim Auto Pilot Cut-Out Switch is at NORMAL and the autothrottle must be engaged.
Correcto Incorrecto Correct answer

Correcto
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Pregunta 54 de 62
54. Pregunta
The Altitude Alerting system consists of a momentary tone and illumination of the Altitude Alert lights when approaching the selected altitude. The alert will occur when
Approaching 500 feet of the selected altitude and the lights will extinguish at 250 feet from the selected altitude.
Correcto Incorrecto Correct answer

Approaching 750 feet of the selected altitude and the lights will extinguish at 100 feet from the selected altitude.
Correcto Incorrecto Correct answer

Approaching 900 feet of the selected altitude and the lights will extinguish at 300 feet from the selected altitude.
Correcto Incorrecto Correct answer

Correcto
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Pregunta 55 de 62
55. Pregunta
If the autothrottle disengagement light is flashing amber, this indicates
An autothrottle airspeed error if speed is not held within +10 or -5 knots of commanded speed when in flight, flaps not up and autothrottle engaged in MCP SPD or FMC SPD mode.
Correcto Incorrecto Correct answer

The light test switch is being held in position 2.
Correcto Incorrecto Correct answer

An autothrottle airspeed error if speed is not held within +15 or -15 knots of commanded speed when in flight, flaps up and autothrottle engaged in MCP SPD or FMC SPD mode.
Correcto Incorrecto Correct answer

Correcto
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Pregunta 56 de 62
56. Pregunta
During a dual channel approach the autothrottle
Automatically disengages approximately 2 seconds after the landing touchdown.
Correcto Incorrecto Correct answer

Automatically disengages approximately 10 seconds after the landing touchdown.
Correcto Incorrecto Correct answer

Must be disengaged manually.
Correcto Incorrecto Correct answer

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Pregunta 57 de 62
57. Pregunta
If the autopilot is engaged and either pilot’s control wheel Trim Switch is activated
The autopilot will disengage.
Correcto Incorrecto Correct answer

The stabiliser will not move and the autopilot remains engaged.
Correcto Incorrecto Correct answer

The stabiliser will move at a slow rate with the autopilot remains engaged.
Correcto Incorrecto Correct answer

Correcto
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Pregunta 58 de 62
58. Pregunta
Autothrottle takeoffs
May be performed with both PMCs ON or both PMCs OFF.
Correcto Incorrecto Correct answer

May be performed with any combination of PMCs.
Correcto Incorrecto Correct answer

May only be performed with both PMCs ON.
Correcto Incorrecto Correct answer

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Pregunta 59 de 62
59. Pregunta
VNAV mode is terminated by
Selecting a different pitch mode or Glideslope capture or Extending the wing flaps beyond 15 degrees.
Correcto Incorrecto Correct answer

Selecting a different pitch mode or Localiser capture or Extending the wing flaps beyond 5 degrees.
Correcto Incorrecto Correct answer

Selecting a different pitch mode or Glideslope capture or De-selecting LNAV or Extending the wing flaps beyond 25 degrees.
Correcto Incorrecto Correct answer

Correcto
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Pregunta 60 de 62
60. Pregunta
If the MCP displayed altitude changes without altitude selector movement
No warnings are given.
Correcto Incorrecto Correct answer

A warning will be given in the form of intermittent altitude alert tone, flashing altitude alert lights and the MCP displays 50,000 feet.
Correcto Incorrecto Correct answer

A warning will be given in the form of the aircraft climbing or descending to the new altitude.
Correcto Incorrecto Correct answer

Correcto
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Pregunta 61 de 62
61. Pregunta
When approaching a selected altitude in CWS P (pitch) with the autopilot engage paddle in CMD
The CWS P annunciation changes to ALT ACQ and when at the selected altitude, ALT HOLD engages.
Correcto Incorrecto Correct answer

The autopilot paddle automatically moves to the CWS position on reaching the selected altitude.
Correcto Incorrecto Correct answer

The CWS P annunciation is unaffected.
Correcto Incorrecto Correct answer

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Pregunta 62 de 62
62. Pregunta
The recommended Autothrottle approach speed setting is
VREF + 10 knots.
Correcto Incorrecto Correct answer

VREF + 5 knots.
Correcto Incorrecto Correct answer

VREF + increments due to wind or gusty conditions.
Correcto Incorrecto Correct answer

Correcto
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Automatic Flight B737NG

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31. Pregunta

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35. Pregunta

36. Pregunta

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38. Pregunta

39. Pregunta

40. Pregunta

41. Pregunta

42. Pregunta

43. Pregunta

44. Pregunta

45. Pregunta

46. Pregunta

47. Pregunta

48. Pregunta

49. Pregunta

50. Pregunta

51. Pregunta

52. Pregunta

53. Pregunta

54. Pregunta

55. Pregunta

56. Pregunta

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60. Pregunta

61. Pregunta

62. Pregunta