Engines and APU Flashcards
N1 is the _____ pressure compressor and is a primary engine indication.
low
N2 is the _____ pressure compressor and is a secondary engine indication
high
The Start Levers positions are ______.
IDLE and CUTOFF
Reverse thrust cannot be selected unless ______.
the forward thrust lever is at IDLE
Positioning an engine Start Lever to CUTOFF closes the ______.
respective Spar and Engine Fuel Shutoff Valves
The ______ compares commanded N1 to actual N1 and adjusts fuel flow to achieve commanded N1
Electronic Engine Control (EEC)
The Electronic Engine Control (EEC) in either normal or alternate mode DOES NOT provide ______ protection.
EGT redline
In Normal Mode, the Electronic Engine Control (EEC) uses ______ conditions and _______ to calculate N1 thrust ratings.
sensed flight/bleed air demand
If an Engine EEC switch has both ON (white) and ALTN (amber) displays illuminated, the engine is operating in __________ mode.
either SOFT or HARD alternate
If an ENGINE CONTROL (amber) light illuminates ______
there is a non-dispatchable fault in the Engine Control System.
The Thrust Mode Display indicates R-TO (green). What mode is active?
Reduced Takeoff Thrust
What causes the ENG FAIL Alert (amber) on the EGT indicator?
N2 drops below 50% and start lever is in IDLE
What removes an ENG FAIL Alert (amber)
All of the above
On the ground after engine shutdown a red box around the EGT Readout indicates _______.
an in-flight exceedance has occurred.
“Reverse video” displayed on the Engine Vibration readout indicates _______.
high engine vibration level