61-80 Flashcards
After completing the memory item and QRC for a hot start, what section of the QRH will you reference for an Engine Abnormal Start?
Non-Annunciated
Departing SFO on 1R, you experience and engine failure at V1. You accomplish the actions and callouts according to the SOPM and upon reaching VFS, you call, “Continuous, Bank Off.” How is engine thrust set to “continuous?”
Select the TRS key on the MCDU then select “CON.”
When the PF advances the thrust levers to the TO detent and calls ‘‘Check Thrust” the PM should verify?
N1 has reached target
ATTCS is green
engine parameters normal
On final approach, you notice that GA mode is displayed between the N1 gauges. What immediate pilot action is required?
None, this is normal after gear and flaps are extended
The use of Flex Thrust for takeoff is prohibited during the following conditions:
Windshear reported or forecast
In the SOPM, what guidance is given regarding thermal stabilization before shutting down either engine?
Both engines must run at or near idle for two minutes prior to shutdown
With the thrust levers set to TO, when will ATTCS command RSV thrust?
All answers are correct:
difference between both engine N1 values exceeding 15%
windshear detection
engine failure during takeoff
go-around
If you choose NOT to dry motor an engine after the first failed start attempt, how long must you wait before the second engine start is attempted?
10 seconds
If FADEC automatically aborts a failed engine start attempt, why must the pilot perform the ENGINE ABNORMAL START memory item?
The Starter Control Valve must be manually closed to ensure the
starter limitation will not be exceeded.
The engine start must be manually aborted when:
1) no positive oil pressure indication within 10 seconds after N2 increase
2) Oil pressure below limits
3) a positive increase of N1 is not indicated prior to starter cutout
4) N1and/or N2 failing to accelerate to stable idle speed (hung start).
5) No ITT light off within 30 seconds of engine start
6) ITT exceeds start limit (815°C- Hot)
7) An intermittent electrical, pneumatic, or starter malfunction
Which of the following statements are true about the stick shaker?
The autopilot is automatically disconnected at shaker activation
After starting Engine #1, the Captain calls for, “Flaps 2, APU off, flight control check.” Which statement is TRUE regarding the flight control check?
All statements are correct:
elevators, ailerons and rudders indicate travel in correct directions
flight controls are checked for freedom of movement
a full green box indication on the synoptic page is not a requirement
What is the purpose of the Electrical Power-Up Built In Test (PBIT)?.
Provides detection of out-of-tolerance conditions and failures in the FCMs, P-ACEs, and SF-ACEs
During your Origination flow, you accidentally interrupt the electric PBIT. You should:
As long as the “FLT CTRL BIT EXPIRED” message is not displayed and you have enough time remaining to takeoff, no further action is required
On the first flight of the day with an OAT of -20° Celsius, you notice an “AFCS FAULT” message displayed on the EICAS along with erroneous airspeed indications on the PFDs. What action should you take?
Turn the ADSP Heater Switch to ON, allow the E-PBIT to run properly, and ensure the AFCS FAULT message is no longer displayed.
