Study Guide: Warning Systems Flashcards
757/767: Altitude alerting is inhibited:
In flight with all landing gear down and locked
757/763: According to the graphic, when the CANCEL switch is pushed it:
Cancels caution and advisory messages
757/763: The status cue (STATUS) displays on the upper left corner of the secondary EICAS display when a new status message exists. The new status message is displayed
by:
Pushing the STATUS DISPLAY switch
757/767: An overspeed warning occurs if VMO/MMO limits are exceeded. One of the
indications includes an aural warning siren. How can the aural warning siren be silenced?
By pushing either master WARNING/CAUTION reset switch
757/767: The master WARNING lights and fire bell are inhibited:
From nose gear extension during rotation until 400 feet AGL or 20 seconds elapsed time, whichever occurs first
757/767: The master CAUTION lights and aural beeper are inhibited:
From 80 knots until 400 feet AGL or 20 seconds elapsed time, whichever occurs first
757/767: Takeoff configuration warning messages include:
Flaps, parking brake, spoilers, stabilizer
757/767: The landing configuration warning system alerts pilots that the landing gear is not extended for landing. The landing configuration warning activates if the aircraft is in
flight, any landing gear is not down and locked and:
Either the flaps are in a landing position (25 or 30) or any thrust lever is at idle below 800 feet RA
757/767: If the left radio altimeter fails, the configuration warning for gear not down with either throttle in idle can occur:
At any altitude
757/767: When deviating from MCP altitude by ____ feet the master CAUTION lights illuminate, aural alert sounds and EICAS caution ALTITUDE ALERT is displayed.
300
757/767: At _______ prior to reaching the selected MCP altitude, the ALT lights illuminate on each pilot’s altimeter.
900 feet
757/767: An overspeed warning occurs if VMO/MMO limits are exceeded. All warning indications remain activated until:
Airspeed is reduced below VMO/MMO
757/767: Existing takeoff configuration warnings are terminated at liftoff or cancelled:
When the configuration error is corrected
757/763: How can engine indications be displayed in the event that both CRTs or both
EICAS computers fail?
The standby engine indicator (SEI) automatically activates