Term
Which systems do the DCU's provide data to? |
|
Definition
EICAS displays aural warnings (not TWAS and TCAS flight data recorder mx diagnostic computer lamp driver units |
|
|
Term
What emergency function is incorporated in the reversionary control panel? |
|
Definition
Pushing all 3 Tune Inhibit buttons tunes COMM 1 to 121.5 |
|
|
Term
Which displays do you lose in EICAS compressed format? |
|
Definition
Radio tuning data ITT and N2 digital readouts pressurization data cabin temp crew oxygen pressure individual fuel tank quantity |
|
|
Term
Which indications only appear on the summary page? |
|
Definition
Engine fuel temp and 10th stage bleed pressure |
|
|
Term
What does a red X" across the CAS mean?" |
|
Definition
CAS function of both DCUs has failed |
|
|
Term
|
Definition
DCUs disagree for a particular message or aural alert |
|
|
Term
|
Definition
One DCU is not cross-checking engine data |
|
|
Term
What % N1 does the takeoff configuration warning occur? |
|
Definition
|
|
Term
Which systems activate a takeoff configuration warning? |
|
Definition
Autopilot, Brakes, Flaps, Spoilers, Trim |
|
|
Term
When are caution messages inhibited during takeoff? |
|
Definition
Aircraft is on the ground Both engines are > 79% N1 and Airspeed > 80 kts |
|
|
Term
When are inhibited caution messages removed after takeoff? |
|
Definition
Altitude > 400' or Both engines < 79% N1 or 30 seconds after the messages were inhibited |
|
|
Term
When are caution messages inhibited for landing? |
|
Definition
Aircraft is in the air any gear is down and locked and altitude isĀ < 200' RA |
|
|
Term
When are inhibited caution messages removed after landing? |
|
Definition
RA > 200' or 30 seconds after WOW or 90 seconds after messages were inhibited |
|
|
Term
Which aural alerts cannot be silenced? |
|
Definition
EGPWS, TAWS, stall warning, overspeed, trim clacker, takeoff configuration, autopilot cavalry charge, gear horn, altitude alert C-chord, vertical track alert, SELCAL |
|
|