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Flashcards in Autoflight Deck (49)
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30

What pitch and roll commands does the Flight Director provide during T/O?
A. V2 + 15 kts or the speed at rotation plus 15 kts whichever is greater.
B. Heading to maintain the track existing at 5 ft RA after rotation.
C. If target speed is exceeded for 5 seconds, a new target speed up to V2 + 25 kts max.
D. All of the above.

D. All of the above.

31

During climb, if CLB DIR is selected, all altitudes between the airplane altitude and the lower of the MCP or FMC cruise altitude will be deleted.
A. True
B. False

A. True

32

During autoland operations, which of the following occurs at 1500 ft AGL?
A. Self test of autoland system.
B. Only 2 autopilots electrically isolate.
C. LAND 2 or 3 annunciated on the ASA (Rollout and Flare annunciated as armed).
D. A and C.

D. A and C.

33

A flight director mode failure, in either pitch or roll, causes the respective ____ to disappear.
A. Steering bar
B. Flight director
C. TO / GA annunciation
D. None of the above

A. Steering bar

34

With the autothrottle FMA indication of THR REF, the thrust is set to ___ A. MCT
B. Takeoff Power
C. The selected thrust limit displayed on the EICAS.
D. None of the above

C. The selected thrust limit displayed on the EICAS.

35

During the takeoff roll prior to lift off, if the autothrottles are not engaged by ___ they cannot be engaged until above 400 feet AGL.
A. 80 kts
B. 100 kts
C. 50 kts
D. None of the above

C. 50 kts

36

The Mode Control Panel (MCP) provides input to:
• The autopilot only.
• The autopilot and flight director only.
• The flight director only.
• The autopilot, the flight director, and the autothrottles.

• The autopilot, the flight director, and the autothrottles.

37

What display indicates positive engagement of a mode selected on the MCP?
• The Flight Mode Annunciator.
• The light in the switch on the MCP.
• The EICAS display.
• The flight control synoptic.

• The Flight Mode Annunciator.

38

Which of the following statements are correct regarding the Climb/Continuous (CLB/CON) Thrust Switch on the MCP?
A. Selecting CLB/CON with two engines operating selects FMC climb thrust.
B. Selecting CLB/CON with one engine operating selects max continuous thrust.
C. Selecting CLB/CON is not necessary after an engine failure at cruise altitude if ENG OUT is executed on the VNAV CRZ page of the CDU.
D. All the above.

D. All the above.

39

With an EICAS advisory message NO LAND 3 displayed, which of the following is true?
• An ILS approach to CAT Ill minimums should not be attempted.
• CAT Ill operations are not affected.
• ILS minimums are not affected.
• A CAT Ill approach and autoland can be safely conducted to LAND 2 minimums if supported by airport and aircrew requirements.

• A CAT Ill approach and autoland can be safely conducted to LAND 2 minimums if supported by airport and aircrew requirements.

40

Approaches flown using IAN procedures:
• require a ground based glide path transmitter.
• require that raw data be monitored.
• require either a VOR or LOC transmitter for roll guidance.
• always use FMC computed glide path for vertical path guidance.

• always use FMC computed glide path for vertical path guidance.

41

Autoland capability is available for ILS, GLS and IAN approaches.
A. True
B. False

B. False

42

During a low visibility takeoff using HUD guidance, lateral guidance is provided using
A. ILS signals
B. GLS signals
C. LNAV guidance
D. Both A or B

D. Both A or B

43

When using HUD guidance for takeoff, the guidance cue becomes active as the aircraft approaches the centerline and __ .
• is within 45 degrees of runway heading
• is within 90 degrees of runway heading
• is within 5 degrees of runway heading
• is within 30 degrees of runway heading

• is within 45 degrees of runway heading

44

If the autopilot remains engaged below 100ft RA on an IAN approach, __ is displayed.
• LAND 2
• the Master Warning
• Go-Around
• NO AUTOLAND

• NO AUTOLAND

45

To use IAN procedures, flight crews should use the ____ mode to enable the approach.
• LOC
• APP
• LNAV
• VOR

• APP

46

On an Autopilot Go-Around, TO/GA to LNAV engages the LNAV function at a minimum altitude of
• 500 ft RA
• 1000 ft RA
• the ACCEL height entered on T/O REF pg. 2
• 200 ft RA

• 200 ft RA

47

During a HUD Low Visibility takeoff, the roll bar on the PFD can be used for lateral guidance.
A. True
B. False

B. False

48

Maximum capture angle for LOC or FAC cannot exceed ____ degrees
• 90
• 45
• 135
• 120

• 120