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The Bank Pointer indicates bank angle. It fills and turns amber if bank angle is 35 degrees or more.

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The white position trend vector with (dashed lines) is displayed in MAP and MAP CTR. Predicts position at the end of 60, 90, and 120 second intervals.

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Predicts position at the end of 30, 60, and 90 second intervals. Each segment represents 30 seconds. Based on bank angle and ground speed.

On which CDU is the ground speed displayed?

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If you select the "BOTH ON 1" switch of the CONTROL PANEL:

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If the FAULT light on the IRS Mode Selector Unit illuminates, what does it indicate?

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If a DEU fails prior to engaging the second autopilot for a dual autopilot approach, engagement of the second autopilot is only possible above 1,500 feet AGL.

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If a DEU fails prior to engaging the second autopilot for a dual autopilot approach, the engagement of the second autopilot is inhibited.

STA (station) displays all FMC data base navigation aids if on map scales ______.

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The white position trend vector with (dashed lines) is displayed in MAP and MAP CTR. Selected range determines the number of segments displayed. For a range of more than 20 nm, there are 3 segments. For a range of 20 nm, there are 2 segments. For a range less or equal than 10 nm, there is only 1 segment.

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The Expanded Localizer Scale is displayed when the autopilot or flight director is in LOC mode, deviation is:

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When penetrating turbulence:

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The standby attitude indicator provides attitude information that is independent of the primary attitude displays. The indicator is powered by:

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The indicator is powered by the battery bus and remains powered after the loss of all normal AC power as long as battery power is available. The gyro reaches operational speed approximately 60 seconds after power is applied.

The ND Wind direction-speed and wind arrow is:

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The Static Air temperature is displayed on:

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The FMC Alerting Message "VERIFY POSITION" indicates:

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Display System Annunciations - When there is a problem with the DEU display system, and when CDS MAINT is shown in white in the lower left corner of the PFD:

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Should the CDS FAULT be displayed in amber, it would mean that a non-dispatchable CDS fault had occurred. Displayed on the ground only, prior to start of the second engine.

The V2+15 white bug of the airspeed indicator is normally displayed for takeoff. It is removed:

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Weather Radar Annunciations (expanded and center MAP, expanded APP, expanded VOR modes) - What does the amber WXR WEAK indicate?

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AOA Disagree Alert (amber) - It indicates the Captain’s (left) and First Officer’s (right) angle of attack values disagree by:

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The amber crosshatched area indicates:

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Weather Radar Annunciations (expanded and center MAP, expanded APP, expanded VOR modes) - What does the amber WXR ATT indicate?

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EFIS Control Panel - Pushing the WXR (weather radar) switch energizes the weather radar transmitter and displays weather radar returns in _____.

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Airspeed Disagree Alert (amber) - Indicates the Captain’s and First Officer’s airspeed indications disagree by:

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The bottom of the red and black bar indicates the:

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On the FMC TAKEOFF REF Page, the SEL temperature entry may be made in either degrees Celsius or Fahrenheit:

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The current Mach number is displayed when airspeed increases above ___ Mach.

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It blanks when airspeed decreases below 0.40 Mach.

The flight recorder OFF Light (amber) is illuminated. What does this indicate?

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What is the purpose of the Air Data Modules (ADMs)?

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There are 4 ADMs. They convert pneumatic pressure to electrical signals and send these data to the ADIRUs. Each pitot air data module is connected to its on-side pitot probe. There is no cross connection.

Concerning Navigation Display Information, Heading is supplied by Air Data Inertial Reference System (ADIRS) and Track is supplied by the FMC during normal operation.

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When the ROLL amber flag appears on the Attitude indicator, Captain’s and F/O’s roll angle displays differ by more than:

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EFIS Control Panel - WXR (weather radar): when the 640 nm range is selected, weather radar returns are limited to:

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The Slip-Skid Indication displaces beneath the bank pointer to indicate slip or skid. It turns amber if:

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It fills amber if the slip-skid indication is also at full scale deflection.

WPT (waypoint) – displays the waypoints in the FMC data base which are not in the flight plan route if the selected range is:

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With the CONTROL PANEL select switch on the DISPLAYS Source Panel in the BOTH ON 2 position:

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An airspeed trend vector indicates predicted airspeed in:

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Magnetic-True Heading is annunciated in green. When TRU is displayed and the airplane descends _____, an amber box is drawn around TRU. The box flashes for 10 seconds, then turns steady amber.

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Selection of an ILS approach from a DEP-ARR page will automatically remove a previously selected approach:

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Top of the red and black bar indicates the speed at which:

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The ND wind direction-speed and wind arrow is displayed:

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If the Upper Display fails:

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There is no automatic switching for a lower DU failure.

The standby radio magnetic indicator (RMI) displays magnetic heading and VOR-ADF bearing to the station. The RMI is powered by:

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The RMI is powered by the AC standby bus and remains powered after the loss of all normal AC power as long as battery power is available.

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The rising runway is displayed when localizer pointer is in view and radio altitude is less than ____ feet.

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Reduced maneuver capability exists when operating within the amber regions below the minimum maneuver speed or above the maximum maneuver speed. During non-normal conditions the target speed may be below the minimum maneuver speed.

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The purpose of the FMC LEGS page is to display the lateral and vertical flight path details for each waypoint and to make route modifications involving a portion of a route segment.

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During PATH DESCENT and below the speed restriction altitude, the FMC "OVERSPEED DISCONNECT" alerting message is displayed. What does this indicate?

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The flight crew shall manually reduce speed and reengage VNAV.

The Landing Altitude Reference Bar is displayed vertically and it indicates height above touchdown. The bar is white between ______ above landing altitude and it is amber between ______ above landing altitude.

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Vertical speed is displayed in white and it shows vertical speed when greater than _____. The display is located above the vertical speed indication when climbing and below when descending.

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The altitude range arc (also called "the green banana" by Boeing pilots) is displayed in MAP and MAP CTR modes. It indicates the approximate map position where the MCP altitude will be reached. It is based on:

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When flaps are up, the bottom of the amber bar indicates the:

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This airspeed provides 1.3g maneuver capability to high speed buffet (or an alternative approved maneuver capability set in the FMC maintenance pages). The bar may be displayed when operating at high altitude at relatively high gross weights.

On ground, the PERF DEFAULTS INVALID alerting message is displayed. What does this indicate?

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Maintenance shall be called.

Pitch Limit Indication is displayed in amber and it indicates pitch limit (stick shaker activation for existing flight conditions). It is displayed when:

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To climb to FL280 in the shortest distance, MAX ANGLE should be selected on this page:

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If a DEU fails above FL220:

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The Altitude Disagree Alert indicates the Captain’s and F/O’s altitude indications disagree by:

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Boeing 737NG – Flight instruments