Boeing 777 Auto Flight

1 / 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.

2 / 15

What action resets the autopilot system and warning system, and cancels the AUTOPILOT DISC message?

Pushing the autopilot disconnect switch a second time.

Pushing the CANCEL switch below the master warning switch.

Pushing the CANCEL/RECALL switch a second time.

Pushing the master warning switch when the light is illuminated.

3 / 15

When V/S shows in the V/S-FPA window, what are the correct steps to make a 2.6 degree FPA descent?

Set new altitude, push VS/FPA switch, set 2.6 degree flight path angle.

Push V/S FPA reference switch, set new altitude, push VS/FPA switch, set 2.6 degree flight path angle.

Push VS/FPA switch only.

Push VS/FPA switch, set 2.6 degree flight path angle, set new altitude.

4 / 15

What switch engages the autothrottle with A/T ARM switches in ARM?

APP switch.

CLB/CON switch.

LNAV switch.

A/T engage switch.

5 / 15

What is the sequence of steps to use FLCH to climb to FL250 at 280 kts?

Set FL280 in the ALTITUDE window, push FLCH switch, then set 250 kts in the IAS/MACH window.

Set 280 kt in the IAS/MACH window, push FLCH switch, then set FL250 in the ALTITUDE window.

Set FL250 in the ALTITUDE window, push FLCH switch, then set 280 kts in the IAS/MACH window.

Push FLCH switch, set FL250 in the ALTITUDE window, then set 280 kts in the IAS/MACH 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 does the AUTOPILOT EICAS message mean when an amber line is drawn through the pitch mode on the FMA.

The pitch mode has failed.

The autopilot has entered envelope protection.

The autopilot is operating in a degraded mode and the pitch mode has failed.

All of the answers.

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

When is TOGA armed?

When below 1500 feet RA.

When the landing gear is down.

When G/S is armed.

When flaps are not up.

10 / 15

IAS-MACH Window - The display range is:

120 – 390 KIAS and 0.40 – 0.95 Mach.

0 – 395 KIAS and 0.45 – 0.99 Mach.

100 – 399 KIAS and 0.40 – 0.95 Mach.

100 – 390 KIAS and 0.40 – 0.96 Mach.

11 / 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.

12 / 15

IAS-MACH Window - The selected speed is displayed as the PFD selected speed. Displays 200 knots when power is first applied.

True.

False.

13 / 15

Which AT ARM switch configuration causes the AUTOTHROTTLE R message to display?

Left switch ON, right switch OFF.

Left switch OFF, right switch OFF.

Left switch OFF, right switch ON.

Left switch ON, right switch ON.

14 / 15

An EICAS message is displayed for any fault which limits the capability of the automatic landing system. Aural alerts for EICAS messages not affecting safety of flight are inhibited until after touchdown. Changes in autoland status below 300 feet, other than a transition to NO AUTOLAND status, are inhibited.

True.

False.

15 / 15

Climb-Continuous (CLB-CON) Thrust Switch - On the ground and below _____ feet during takeoff, the switch is inoperative.

400 ft.

500 ft.

300 ft.

250 ft.

Your score is

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Boeing 777 Auto Flight

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