AUTOPILOT Flashcards
What vertical speed does FLC give you in a descent above 12,000 feet?
2,000 FPM.
Reference: OM Vol.2, Section 2-19, Autopilot
Heading mode, Low Bank will give lateral guidance restricted to a maximum bank angle of ____.
14°.
Reference: OM Vol.2, Section 2-19, Autopilot
When pressing the TOGA buttons on the ground while taxiing:
TO mode is activated on the flight director.
Reference: OM Vol.2, Section 2-19, Autopilot
What is the minimum engagement height for the autopilot (feet)?
500’ AGL.
Reference: OM Vol.2, Section 2-19, Autopilot
On non-XR aircraft above 12,000 in FLC, the aircraft climbs at what speed?
270 KIAS until MACH 0.56.
Reference: OM Vol.2, Section 2-19, Autopilot
Which button should be pressed to display FMS course data on the PFD?
FMS.
Reference: OM Vol.2, Section 2-19, Autopilot.
Full bank is equal to _______ degrees?
27°.
Reference: OM Vol.2, Section 2-19, Autopilot
At what altitude must the autopilot be disengaged on a CAT I ILS approach?
200’ AGL.
Reference: OM Vol.2, Section 2-19, Autopilot
The aircraft heading must be within ___ degrees of the final approach course (front course) prior to selecting the APR or NAV mode.
90°.
Reference: OM Vol.2, Section 2-19, Autopilot
What actions will disconnect the autopilot?
Pilot actuation of either of the pitch trim switches, the ‘AP’ or ‘YD’ button on the Flight Guidance Control Panel’, pressing the quick disconnect button.
Reference: OM Vol.2, Section 2-19, Autopilot.
During climb, FLC works just like.
IAS/Mach but with preset speeds.
Reference: OM Vol.2, Section 2-19, Autopilot
True/False: The yaw damper is automatically turned on when the autopilot is engaged.
True.
Reference: OM Vol.2, Section 2-19, Autopilot
What pitch attitude does the GA flight guidance mode present immediately after being armed (airspeed above the white band of the low speed awareness tape)?
10°.
Reference: OM Vol.2, Section 2-19, Autopilot
The flight-guidance DES mode is programmed to function like.
VS mode but with preset vertical speeds.
Reference: OM Vol.2, Section 2-19, Autopilot
Crews must always verify that the autopilot is coupled to the PF by looking at the ___________.
Flight Mode Annunciator (FMA).
Reference: OM Vol.2, Section 2-19, Autopilot