Automatic Flight B737NG

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

The underspeed symbol in the MCP Speed window is a

The Automatic Flight System (AFS) provides speed, pitch and thrust commands to avoid exceeding the following limit speeds

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

During a dual channel autopilot approach, the Autopilot Disengage light illuminates steady red when below 800 feet. This indicates

Which radio altimeter provides radio altitude to the autothrottle

VNAV climbs and descents are

During an autopilot go-around, the Autopilot Disengage light illuminates steady red. This indicates

Dual channel Autopilot operation is possible

When intercepting the ILS with APP mode armed

If the autothrottle is engaged and an autothrottle disengage switch is pressed

Dual autopilot engagement is possible

The Autothrottle sets take-off thrust prior to

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

What is the minimum Mach number that can be selected in the IAS/MACH display of the MCP panel

After LOC and G/S are both captured, the APP mode can be exited by

During a single Autopilot approach, a Go-around is initiated by pressing a TOGA button. This causes

During a Dual Channel Autoland Approach, the autopilots were disengaged at 200 feet RA and

If FLARE arm is not annunciated by approximately 350 feet radio altitude

During Autopilot CWS operation above 1500 feet RA, if the roll control force is released with less than 6 degrees of bank, the autopilot will

If the Autothrottle is engaged during a touchdown

The Autothrottle is engaged in FMC speed mode. What is displayed in the IAS/MACH display of the MCP

The mode selector switches on the MCP panel will illuminate the letters ON to indicate that

When operating in “ALT HOLD”, the V/S mode is ARMED if the MCP altitude is changed by more than

During a dual channel go-around, the MCP IAS/Mach display will

If the MCP selected Altitude is changed during ALT ACQ mode

The A/P go-around mode requires dual A/P operation and becomes armed when

The aircraft is climbing with the autopilot in CMD and the pilot pushes the control column forward. The autopilot will

Flight Director roll commands, from take-off mode engagement through to the take-off climbout, are

During a single engine F/D go-around

The conditions for engaging the flight director in go-around mode are

A rectangle is drawn around each pitch, roll, CWS and thrust engaged mode annunciation (EFIS Flight Mode Annunciations) whenever

During an ILS approach with both flight directors ON

The Flight Director Comparator monitors

Both MA lights on the MCP panel are illuminated during an approach indicating

The STAB OUT OF TRIM light operates

The Altitude Alerting system is inhibited whenever

All AFDS modes can be disengaged by selecting another command mode or

A takeoff is commenced with both Flight Directors selected OFF. At 100 knots IAS a TOGA switch is pressed. What will happen to the F/D ?

If the autopilot disengage light is flashing amber, this indicates that

If an engine fails while the autothrottle is in N1 mode, the thrust lever of the failed engine

What criteria must be met before autopilot engagement

The Altitude Alerting system consists of a momentary tone and illumination of the Altitude Alert lights when approaching the selected altitude. The alert will occur when

If the autothrottle disengagement light is flashing amber, this indicates

During a dual channel approach the autothrottle

VNAV mode is terminated by

If the MCP displayed altitude changes without altitude selector movement

When approaching a selected altitude in CWS P (pitch) with the autopilot engage paddle in CMD

The recommended Autothrottle approach speed setting is