Flt Warning Systems Flashcards
A rectangular symbol [ ] prefaces an EICAS alert message that has an associated checklist…
- that has been completed.
- that has procedural steps.
- with no procedural steps or notes or information of which the crew must be made aware.
- that includes Quick Action Items that must first be addressed by using the QRC.
that has procedural steps.
EICAS status messages indicate equipment faults which may affect aircraft…
- non-essential equipment reliability.
- takeoff performance.
- dispatch capability.
- safety of flight.
dispatch capability.
MCP selected altitude alerts are inhibited when glideslope is captured.
- True
- False
True
In addition to NO AUTOLAND and TAMS, four time critical warnings are displayed in red on the lower portion of the Primary Flight Display (PFD) and are also displayed on the upper portion of the HUD. Which of the following alerts is NOT displayed on the PFD or the HUD?
- SPEEDBRAKE
- ENG FAIL
- PULL UP
- TERRAIN
TERRAIN
EICAS memo messages are crew reminders of certain flight crew selected normal conditions. E.g. PARKING BRAKE SET. Memo messages…
- display by pushing the CANC/RCL switch when the last page of EICAS alert messages is displayed.
- can be cancelled by pressing the CANC/RCL switch.
- are displayed in CYAN.
- have priority over alert messages.
display by pushing the CANC/RCL switch when the last page of EICAS alert messages is displayed.
EICAS Communication messages are always preceded by a…
- white rectangular [ ] symbol.
- white dot.
- amber dot.
- one-space indent from previous messages.
white dot.
When EICAS caution or advisory messages are displayed, a single push of the CANC/RCL switch on the Display Select Panel (DSP)…
- displays all pages of EICAS messages when additional pages exist.
- displays the previous page of EICAS messages when a previous page exists.
- cancels all displayed warning messages.
- displays the next page of EICAS messages when additional pages exist.
displays the next page of EICAS messages when additional pages exist.
Predictive Windshear (PWS) alerts are enabled approximately 12 seconds after weather radar begins scanning for windshear.
- True
- False
True
In flight, Predictive Windshear (PWS) alerts are enabled…
- below 2300 feet radio altitude.
- below 1200 feet radio altitude.
- 12 seconds after descent below 1200 feet radio altitude.
- below 1500 feet radio altitude.
below 1200 feet radio altitude.
A TCAS resolution advisory (RA) is indicated on both the navigation display and mini-map as a…
- filled white diamond.
- filled red square.
- unfilled white diamond.
- filled amber square.
filled red square.
The EICAS caution message ALTITUDE ALERT is displayed and a highlighted amber box is displayed around the current altitude when departing the selected altitude by…
- 500 feet.
- 250 feet.
- 300 feet.
- 200 feet.
200 feet.
Like the other three time critical warnings displayed on both the PFD and HUD, the Speedbrake Warning is also accompanied by a Master WARNING light and an aural alert. “SPEEDBRAKE, SPEEDBRAKE” alerting the crew that…
- the speedbrake has not deployed during landing or during a rejected takeoff.
- the speedbrake is deployed with flaps in the landing configuration.
- the speedbrake is not armed for landing.
- the speedbrake lever is extended beyond ARMED below 800 feet - altitude.
the speedbrake has not deployed during landing or during a rejected takeoff.
What will cause the CONFIG GEAR warning in flight with the landing gear not down and locked?
- FLAP lever in landing position.
- GEAR OVRD selected to OVRD on the GPWS page of the TCP.
- Descent below 500 feet - altitude regardless of thrust lever position.
- Nothing.
FLAP lever in landing position.
Thrust Asymmetry Minimum Speed (TAMS), varies with weight and CG but will always be at least ____ knots above minimum control speed during takeoff or go-around.
- 20
- 15
- 10
- 5
10
When does the Master CAUTION lights, beeper, and new EICAS caution messages inhibit begin during takeoff?
- At 400’’ RA or 20 seconds after liftoff.
- At 80 knots airspeed.
- Never. All three remain uninhibited throughout takeoff.
- At V1 through 400’’ RA.
At 80 knots airspeed.
Takeoff configuration warnings include master warning lights, activation of the aural warning siren, and display of applicable EICAS warning CONFIG message. Takeoff configuration warnings are inhibited at…
- 80 knots.
- V1 or rotation, whichever occurs first.
- 400’’ RA or 20 seconds after liftoff, whichever occurs first.
- 6 knots prior to V1.
V1 or rotation, whichever occurs first.