ENGINE FIRE INDICATION
When an overheat/fire condition occurs in the
engine nacelle, the fire detection sensing el-
ements activate the detection control unit.
This action causes the following warning in-
dications to occur (Figure 8-2):
• A triple chime sounds and the MASTER
WARN lights flash.
• “FIRE” (red, flashing) annunciates in-
side of the EICAS ITT indicator arc on
the affected engine.
• The affected engine red “FIRE PUSH”
button on the engine/fuel control panel
flashes.
• A voice message announces “Left/Right
Engine fire.”
• If selected, the RMU engine page (EN-
GINE PGE1) displays “FIRE” (red) next
to the N1 analog RPM tape for the af-
fected engine.
Either master WARN light may be depressed
to cancel the master WARN lights, cancel the
voice message and to stop the flashing of the
EICAS “FIRE” annunciator. The EICAS
“FIRE” annunciator and the “FIRE PUSH”
button remain illuminated as long as the over-
LEARJET 45 PILOT TRAINING MANUAL
8-3
FOR TRAINING PURPOSES ONLY
FlightSafety
international
RIGHT ENGINE FIRE, . . ."
LEFT ENGINE FIRE, . . ."
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