|1.- If both ECAM screens fail or are switched off, the E/WD information is: A.- Automatically transferred to the Capt.'s PFD. B.- Lost for the rest of the flight. C.- Displayed on an ND using the ECAM/ND XFR switch.
2.- Actions to be carried out are shown in ____ on the ECAM E/WD. A.- Blue. B.- Amber. C.- Red.
3.- MEMO display is located on the: A.- MCDU. B.- SD memo section. C.- E/WD memo section.
4.- A "To Inhibit" or "LDG Inhibit" memo is displayed in magenta to remind the
crew: A.- The takeoff or landing is inhibited. B.- Most of the failure titles and associated checklists are suppressed. C.- All of the failure titles and associated checklists are suppressed.
5.- When the TO CONFIG key is pushed it: A.- Simulates takeoff power application. B.- Triggers a warning if the airplane is not properly configured. C.- Displays TO CONFIG NORMAL if airplane properly configured. D.- All the above.
6.- Following a failure of the ECAM control panel: A.- The ECAM is lost. B.- System pages can be displayed by pressing the ALL siwitch. C.- The ECAM pages automatically transfer to the ND.
7.- The speed trend arrow on the PFD airspeed scale indicates the speed value
that will be attained in _____ seconds if the acceleration remains constant. A.- 5 B.- 10 C.- 15.
8.- Weather radar can be displayed in what modes on the ND? A.- ARC and ROSE NAV modes only. B.- All modes except plan. C.- ROSE VOR and ROSE ILS modes. D.- ROSE NAV mode only.
9.- If a PFD fails, does anything happen automatically? A.- The ATT HDG switch must be used on the switching panel in order to recover
PFD information. B.- Yes, the image automatically transfers to the display formerly occupied by the
ND. C.- Yes, the image automatically transfers to the UPPER ECAM. D.- No.
10.- The three Display Management Computers (DMCS) acquire: A.- A process all input from airplane sensors and computers to generate the
display images. B.- Data for the display of alert messages, aural alerts, and voice messages. C.- Data for ACARS messages.
11.- The electronic centralized airplane monitoring (ECAM) system presents
data on two identical CRT displays, they are: A.- The PFD and the ND. B.- The ND and the E/WD. C.- The E/WD and the SD.
12.- An "STS" message will flash on the engine/warning display after engine
shutdown to: A.- Alert maintenance. B.- Alert the crew. C.- Remind the crew to turn off the ECAM.
13.- The A-320 Electronic Flight Instrument System (EFIS) consists of ________
identical display units. A.- 4 B.- 6 C.- 8.
14.- The system display (SD) has 12 different system pages that can be
displayed: A.- Automatically. B.- On crew demand. C.- Both A and B.
15.- If the Upper ECAM secreen fails, the E/WD data is: A.- Lost for the rest of the flight. B.- Automatically transferred to the lower screen. C.- Manually transferred to the MCDU.