Warn Flashcards
What action is required to display the next page of the STATUS messages when additional pages exist?
B. Select “NEXT PAGE” on the lower right corner of the Status Page.
The Fire Bell & Master Warning lights are inhibited during takeoff from V1 until 400 ft RA or 25 seconds after V1, whichever occurs first.
A. True
Which statement about Memo Message is true:
A. Memo Messages are not considered crew alerts.
B. Memo Messages are displayed in white font on EICAS.
C. Memo Messages indicate the current state of certain aircraft systems.
The terrain data on the ND is magenta when:
No terrain data is available.
Weather radar are shown on the NAV Display in all modes except:
Plan.
The GPWS provides various warning, caution and advisory level alerts based on ____.
A. Radio altitude, Barometric altitude, Aircraft configuration
C. ADRS, Glideslope Deviation, Weather Radar`
What precaution should be taken if a tail strike occurs during takeoff?
B. The airplane should not be pressurized.
Which of the following would remove a WINDSHEAR time critical warning?
B. Flying out of the windshear condition.
A filled red square on a TCAS alert indicates:
A resolution advisory (RA).
During ground engine start, new caution and advisory alerts are inhibited from engine start switch engagement until:
A. The engine reaches idle RPM.
B. The start is aborted.
The Look-Ahead Terrain Alerting feature includes a caution and warning alert. If neither pilot has terrain selected, how is the information supplied to the pilots.
A. A caution terrain alert is initiated approximately 40-60 seconds from projected impact.
B. A warning terrain alert is initiated approximately 20-30 seconds from projected impact.
C. The terrain data is automatically displayed on the ND with the first alert.
Status messages that appear during flight should be written up in the aircraft logbook with no further action by the flight crew.
A. True
When LAND 2 or LAND 3 are displayed, the master CAUTION lights and beeper for most messages are inhibited below ____ feet AGL.
200
Testing of the Weather Radar anf Predictive Windshear System by the flight crew is required before each flight.
B. False
Which of the following is true of an overspeed condition?
A. The MASTER WARNING lights illuminates.
B. An OVERSPEED EICAS message appears.
C. An aural warning siren sounds, can be cancelled by pushing the aural cancel switch.
An overflow of messages in the EICAS message field is indicated by:
A page cue below the alert field.
Status messsages are displayed on the MFD STATUS display and must be cleared by maintenance before departure.
A. True
Which of the following alert messages can be cleared by the CANCEL / RECALL switch?
Advisory alerts.
To cancel the autopilot disconnect aural alert:
Use the control yoke autopilot disconnect button.
Warning alerts, communication alerts, and memo messages:
A. Cannot be cleared.
Which of the following warning cannot be silenced by the MASTER WARNING / CAUTION reset switch:
A. Takeoff configuration
B. Autopilot disconnected
C. Landing configuration
The look ahead terrain warining display is only available if either pilot has selected TERR on their EFIS control panel.
B. False
An engine may be shut down based on a STATUS message only.
B. False
A beeper is used for all system alert caution messages and a bell is used for fire warnings.
A. True
Takeoff configuration warnings are armed when the aircraft is on the ground and thrust is in the takeoff range on either engine.
A. true
Are EICAS caution alert messges inhibited during takeoff?
Yes, messages are inhibited during T/O. The inhibit ends at 400 ft RA, or 20 sec after rotation, whichever occurs first.
How is EGPWS terrain information generated?
The terrain display information is generated from a database contained in the GPWS computer ad correlated to the GPS position.
The Predictive Windshear System (PWS) is a part of which system?
The Predictive Windshear System (PWS) is a part of the weather radar system.
How can a PILOT RESPONSE messaged be cleared?
The PILOT RESPNSE message can be cleared by pushing any control on any of the monitored systems or panels.
When airspeed has reduced to TAMS (Thrust Asymmetry Minimum Speed), Flight deck indications are ____.
A. An aural warning of “AIRSPEED AIRSPEED” with an associated Master Warning
