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10 Cards in this Set
- Front
- Back
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1. What occurs if the Master Warning/Caution Reset switch is pushed?
A. Both Master WARNING and CAUTION lights extinguish B. Only the EICAS CAUTION message extinguishes C. Both Master CAUTION lights extinguish and the EICAS CAUTION message extinguishes |
A. Both Master WARNING and CAUTION lights extinguish
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2. What switch silences the fire bell?
A. EICAS Cancel switch B. Master Warning/Caution Reset switch C. Maximum Indication Reset switch |
B. Master Warning/Caution Reset switch
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3. When are the fire bell and Master WARNING lights inhibited during takeoff?
A. Begins at an airspeed of 80 knots and ends at either 20 seconds elapsed time since nose strut extension or first penetration of 400 feet radio altitude, whichever occurs first B. The fire bell and Master WARNING lights are never inhibited during takeoff to provide immediate crew awareness and corrective action C. Nose strut extension and ends at either 20 seconds elapsed time or at 400 feet radio altitude, whichever occurs first |
C. Nose strut extension and ends at either 20 seconds elapsed time or at 400 feet radio
altitude, whichever occurs first |
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4. When are the beeper and Master CAUTION lights inhibited during takeoff?
A. At 80 knots and ends at either 20 seconds since nose strut extension or 400 feet radio altitude, whichever occurs first B. Nose strut extension and ends at either 20 seconds elapsed time or at 400 feet radio altitude, whichever occurs first C. The beeper and Master CAUTION lights are never inhibited during takeoff to provide immediate crew awareness |
A. At 80 knots and ends at either 20 seconds since nose strut extension or 400 feet radio
altitude, whichever occurs first |
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5. Which system alert message requires immediate crew awareness and corrective action?
A. Warnings B. Cautions C. Status |
A. Warnings
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6. Which system alert message requires immediate crew awareness and may require corrective
action? A. Warnings B. Cautions C. Status |
B. Cautions
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7. If both EICAS computers fail, what occurs?
A. Standby Engine Indicator is automatically activated provided AUTO is selected B. Standby Engine Indicator is automatically activated provided OFF is selected C. The EICAS message BOTH EICAS COMPUTERS FAIL is displayed |
A. Standby Engine Indicator is automatically activated provided AUTO is selected
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8. If one EICAS screen is inoperative, what occurs if the Status Display switch is selected in flight?
A. The Status messages will display on the remaining screen replacing the engine instruments B. Nothing, the Status page is inhibited until the aircraft is on the ground following a failure of one EICAS screen C. FMC STATUS page 2 of 12 displays Status messages |
B. Nothing, the Status page is inhibited until the aircraft is on the ground following a failure of
one EICAS screen |
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9. What occurs if the upper EICAS CRT fails?
A. Engine indications appear on the lower EICAS CRT B. Engine indications appear on the Standby Engine Indicator C. A DISPLAY INOP EICAS message appears on the upper EICAS CRT |
A. Engine indications appear on the lower EICAS CRT
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10. Should the FMC not detect any crew activity occurring over a set duration of time, a series of
EICAS annunciations will begin. True or False? A. True B. False |
A. True
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