17. In Takeoff mode, what is the minimum and maximum limits for pitch ?

a) Minimum 8 degrees , maximum 18 degrees

18. What has to occur to get the Altitude Hold mode to change to the Glide Slope or VNAV Glide Path mode?

a) The Glide Slope or Glide Path must be armed by pushing the APP button .

20. WSHR activates when:

a ) A windshear warming or caution condition is detected and either TOGA button is pressed , A windshear warning condition is detected and the thrust lever is set to the TOGA position and Automatically when a windshear warning condition is detected and the aircraft is in the TO or GA mode

22. Windshear detection is available at what altitudes?

a) Between 10 feet and 1500 feet AGL

23. What is the function of the red AP / TRIM DISC button on the yoke?

a) Autopilot / Trim system disengagement. b) Stops any active trim command if the button is pushed and held

24. What is the difference between APPR1 and APPR2?

a) APPR1 - CAT I capable b) APPR2 - CAT II capable

26. What does the SRC button do?

a) Alternates between the Captain and the First Officer FMA modes as source for the autopilot b) Displayed as a green arrow

27. What is the retard mode (RETD)? When does it engage?

a) Thrust is reduced to idle during flare on landing and engages at or below 30 ft AGL

28. What does LIM and OVRD mean on the FMA?

a) LIM - Autothrottle authority is not sufficient to achieve or maintain the selected airspeed b ) OVRD - AT can be overridden by moving the thrust levers in any direction without causing its disengagement

29. When is CRZ automatically selected?

a) Leveled at the altitude set on the altitude preselector for 90 seconds b) Airspeed is within 5 kt from the preselected airspeed

a) Flight Path Angle is a Pilot - selectable pitch attitude ( in degrees ) of climb or descent . b) FGCS adjusts thrust and pitch to maintain path angle and airspeed.

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Chapter 3-2

Automatic Flight

Question	Answer
16. The Heading Select mode provides lateral guidance through the use of which control?	a) HDG knob
17. In Takeoff mode, what is the minimum and maximum limits for pitch ?	a) Minimum 8 degrees , maximum 18 degrees
18. What has to occur to get the Altitude Hold mode to change to the Glide Slope or VNAV Glide Path mode?	a) The Glide Slope or Glide Path must be armed by pushing the APP button .
19. GA mode does not transition to ASEL / ALT modes if the selected altitude is within a ______ window from the altitude of the TOGA activation.	a) 400 feet
20. WSHR activates when:	a ) A windshear warming or caution condition is detected and either TOGA button is pressed , A windshear warning condition is detected and the thrust lever is set to the TOGA position and Automatically when a windshear warning condition is detected and the aircraft is in the TO or GA mode
21. When climbing using VNAV, the default sub - mode will always be FLCH. (T / F)	a ) True
22. Windshear detection is available at what altitudes?	a) Between 10 feet and 1500 feet AGL
23. What is the function of the red AP / TRIM DISC button on the yoke?	a) Autopilot / Trim system disengagement. b) Stops any active trim command if the button is pushed and held
24. What is the difference between APPR1 and APPR2?	a) APPR1 - CAT I capable b) APPR2 - CAT II capable
25. What does the green arrow on the FMA indicate?	a) The selected FMA source
26. What does the SRC button do?	a) Alternates between the Captain and the First Officer FMA modes as source for the autopilot b) Displayed as a green arrow
27. What is the retard mode (RETD)? When does it engage?	a) Thrust is reduced to idle during flare on landing and engages at or below 30 ft AGL
28. What does LIM and OVRD mean on the FMA?	a) LIM - Autothrottle authority is not sufficient to achieve or maintain the selected airspeed b ) OVRD - AT can be overridden by moving the thrust levers in any direction without causing its disengagement
29. When is CRZ automatically selected?	a) Leveled at the altitude set on the altitude preselector for 90 seconds b) Airspeed is within 5 kt from the preselected airspeed
30. What is FPA?	a) Flight Path Angle is a Pilot - selectable pitch attitude ( in degrees ) of climb or descent . b) FGCS adjusts thrust and pitch to maintain path angle and airspeed.

Created by: lglippig

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