To climb to FL280 in the shortest distance, MAX ANGLE should be selected on this page:
CLB
When penetrating turbulence:
The Turbulence N1 is a reference only. The autothrottle must be disconnected and the N1 set manually
The purpose of the FMC FIX INFO page is to:
Establish your position relative to any stored fix.
Create a new waypoint at the intersection of the active route and a radial or distance from a known fix
If the FAULT light on the IRS Mode Selector Unit illuminates; it indicates:
A system fault affecting the respective IRS ATT and/or NAV Mode
On the FMC TAKEOFF REF Page, the SEL temperature entry may be made in either degrees Celsius or Fahrenheit:
True.
The FMC Alerting Message ‘VERIFY POSITION’ indicates:
Position information is contradictory.
During PATH DESCENT and below the Speed Restriction Altitude, the FMC Alerting Message ‘OVERSPEED DISCONNECT’ means:
During path descent and above or below the speed restriction altitude, VNAV disengages when airspeed exceeds FMC speed restriction by more than 15 knots.
Using a Reduced Takeoff thrust setting may result in Automatic FMC of Reduced Climb Thrust.
True.
The purpose of the FMC LEGS page is to display the lateral and vertical flight path detailsfor each waypoint and to make route modifications involving a portion of a route segment:
True.
The airplane is not certified for operations:
Above 82°N or below 82°S.
On which CDU is the ground speed displayed?
POS REF page 2.
Selection of an ILS approach from a DEP/ARR page will automatically remove a previously selected approach:
True.
With the CONTROL PANEL select switch on the DISPLAYS Source Panel in the BOTH ON 2 position:
The First Officer’s EFIS Control Panel is supplying identical inputs to the captain’s & First Officer’s displays.
The Slip/Skid indication of the Attitude Indicator will turn amber if bank angle is 35 degrees or more.
Turns amber if bank angle is 35 degrees or more; fills amber if the slip/skid indication is also at full scale deflection.
The rising runway is displayed when localizer pointer is in view and radio altitude is less than ____ feet.
2500.
The Glide Slope Pointer is not displayed when the track and the front course on the Mode Control Panel differ by more than 90 degrees (back course).
True.
The standby radio magnetic indicator (RMI) displays magnetic heading & VOR/ADF bearing to the station. The RMI is powered by:
The AC standby bus.
When the ‘ROLL’ flag (amber) appear on the Attitude indicator:
The Captain & First Officer roll display differ by more than 5 degrees.
The Altitude Disagree Alert (amber ‘ALT DISAGREE’) on the digital altimeter indicates the Captain’s & F/O’s altitude indications disagree by more than:
200 feet for more than 5 continuous seconds.
If the Altitude Failure Flag (amber) appears, it means that the barometric altitude or barometric correction has failed. All altimeter symbols are removed except the ALT
ALERT annunciation and the barometric setting.
True
Concerning Navigation Display Information, Heading is supplied by Air Data Inertial Reference System (ADIRS) & Track is supplied by the FMC during normal operation.
True.
The message EXCESS DATA is displayed if the amount of information sent to the navigation display exceeds the display capability. The message can be removed by:
Reducing the amount of map information.
Reducing range.
Deselecting one or more of the EFIS control map switches (STA, WPT, ARPT, DATA, POS).
If you select the ‘BOTH ON 1’ switch of the CONTROL PANEL:
The Left EFIS control panel controls both pilots’ outboard & inboard display units.
In the air, the flight recorder is not powered if both engines are shut down.
False.
