Autopilot Quiz

The STAB OUT OF TRIM light operates

• Only when the speed trim system is activated.

• Only when the autopilot is engaged.

• At any time.

• Only when autopilot disengaged.

If the autopilot disengage light is flashing Red light OFF, this indicates that

• The autopilot has reverted to CMD pitch or roll while in CWS.

• The autopilot disconnect switch has pressed.

• The light test switch is being held in position 2.

• The autothrottle computer failed.

If the autopilot disengagement light is flashing RED, this indicates

• THE light test switch is being held in position

• Pressing an autopilot disengage switch.

• 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.

• The autothrottle computer failed.

If during a climb with autopilot engaged, the ALT HOLD switch is pressed, the aircraft will

• Continue the climb to the next 1000 feet level and level off.

• Continue the climb to the preset altitude selected, as the altitude acquire mode is now armed.

• Stop the climb and level off.

• Continue to climb.

With autopilot A engaged, the altitude selected on the MCP is referenced to

• The Captain's altimeter.

• The First Officer's altimeter.

• The standby altimeter.

• The Radio altimeter.

VNAV climbs and descents are

• Constrained by the selected cabin altitude.

• Constrained by the selected MCP altitude.

• Not constrained by the selected MCP altitude.

• No Constrained by selected cabin altitude.

Where is location of AFC Accessory unit Computer

• On some airplanes, glideslope may be captured prior to localizer.

• On all airplanes, localizer must be captured prior to glideslope.

• The second autopilot can be engaged.

• Avionic compartment rack E 1 - 3.

The stabilizer Out of Trim light illuminates indicate

• FCC NO Power.

• Stabilizer trim selected.

• Autopilot has been Selected.

• Stabilizer trim out of trim more than 10 second.

The bank angle limit selector sets the limit of bank angle when using

• All roll modes.

• Heading select and VOR modes.

• LNAV and heading select modes.

• VNAV and altitude select modes.

The DFCS ( Digital Flight Control System ) consist of

• Two FCC, IRS and Autothrottlles.

• Two FCC, MCP and Actuator input of flight control.

• Two FCC, MCP, IRS, Actuator input of flight control.

• Both FCC and MCP.