Boeing 777 Auto Flight

1 / 15

With the autopilot engaged and LNAV engaged, what will happen if the last active point is passed?

The autopilot will turn the airplane toward the destination airport.

HDG HOLD will engage.

LNAV will maintain current heading.

LNAV will disengage.

2 / 15

What will the autopilot do if you override the control column?

Engage in HDG HOLD and V/S.

Engage in TRK HOLD and FPA.

Cause both roll and pitch modes to fail.

Disengage.

3 / 15

What switch resets the autothrottle system and cancels the AUTOTHROTTLE DISC message?

Master caution switch.

All of the above.

Autothrottle disconnect switch.

Autopilot disconnect switch.

4 / 15

What is the sequence of steps to reduce airspeed with VNAV engaged, using speed intervention?

Change the IAS/MACH window to the lower airspeed, then push FLCH.

Push the IAS/MACH selector, then change the IAS/MACH window to the lower airspeed.

Change the IAS/MACH window to the lower airspeed, then push the IAS/MACH selector.

Push FLCH, then change the IAS/MACH window to the lower airspeed.

5 / 15

What is the sequence of steps to use FLCH to descent to 5000 feet at 240 kts?

Set 5000 feet in the ALTITUDE window, push FLCH switch, then set 240 kts in the IAS/MACH window.

Set 280 feet in the ALTITUDE window, push FLCH switch, then set 500 kts in the IAS/MACH window.

Push FLCH switch, set 5000 feet in the ALTITUDE window, then set 240 kts in the IAS/MACH window.

Set 240 kts in the IAS/MACH window, push FLCH switch, then set 5000 feet in the ALTITUDE window.

6 / 15

What position should the A/P DISENGAGE bar be in during the MCP preflight?

DOWN to the disengaged position.

UP to the engaged position.

None of the above.

Down to the engaged position.

7 / 15

What doe the AUTOPILOT EICAS message mean when an amber line is drawn through the pitch mode of the FMA?

The pitch mode has failed and the autopilot is continuing to operate.

The engaged autopilot has failed.

The pitch mode has failed and the autopilot is diconnected.

8 / 15

When is TOGA armed?

When G/S is armed.

When below 1500 feet RA.

When flaps are not up.

When the landing gear is down.

9 / 15

Is your bank angle limited to 20 degrees when LNAV is engaged and the BANK LIMIT selector is set to the 20 degree position?

Yes.

No.

10 / 15

What will a second push of the TOGA switch do during the takeoff above 80 knots, with LNAV and VNAV armed?

Engages LNAV and VNAV.

Disarms LNAV and VNAV.

Engages LNAV and disarms VNAV.

Disarms LNAV and engages VNAV.

11 / 15

Vertical Speed-Flight Path Angle (VS – FPA) Window - Displays the selected vertical speed in 100 fpm increments or the selected flight path angle in 0.1 degree increments. The display range is:

VS: -10000 to +10000 fpm and FPA: -7.0 to +9.0 degrees.

VS: -8000 to +6000 fpm and FPA: -9.9 to +9.9 degrees.

VS: -5000 to +5000 fpm and FPA: -9.0 to +9.0 degrees.

VS: -9000 to +6000 fpm and FPA: -7.0 to +7.0 degrees.

12 / 15

What does the AUTOPILOT EICAS message mean when an amber line is drawn through the pitch mode of the FMA?

The engaged autopilot has failed.

The pıtch mode ıs armed.

The pitch mode has failed and the autopilot is disconnected.

The pitch mode has failed and the autopilot is continuing to operate.

13 / 15

What happens to bank angle protection if the AP DISENGAGE bar is selected down?

Bank angle protection becomes proportional to the rate of turn.

Bank angle protection remains engaged.

Bank angle protection is disengaged.

Bank angle protection is reduced by half.

14 / 15

With a LAND 2 indication, the level of redundancy is such that a single fault can cause a significant deviation from the flight path (fail passive).

True.

False.

15 / 15

What does the NO LAND 3 EICAS message mean when FLARE and ROLLOUT armed are displayed on the FMA?

The auto land system does not have redundancy for triple channel auto land.

The autopilot disconnect switch has been pushed.

The autopilot is inoperative. Manual landing is required.

Autoland is not possible.

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Boeing 777 Auto Flight

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