BOMBARDIER BD-100-1A10, Руководство по эксплуатации

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FIRE PROTECTION
Sep 13/2004 Flight Crew Operating Manual Volume 2
REV 1 CSP 100-6
09-01-13
EICAS MESSAGES
The fire protection system CAS messages and voice aurals are listed in the table below. A brief explanation of each message
is provided.
MESSAGE INHIBITS MEANING
AURAL
WARNING
APU FIRE Fire has been detected in the APU compartment
L (R) ENGINE FIRE
The L (R) ENGINE FIRE CAS, FIRE EI in the N1
indicator, FIRE indication in the L(R) ENG FIRE
switch, or “LEFT (RIGHT) ENGINE FIRE’ voice
message indicates that the engine fire detection
loop has activated. An engine fire is usually
accompanied by other indications, such as:
excessive ITT, erratic or rough engine operation,
fluctuating engine indications, or smoke in the
cabin.
“Left (Right)
Engine Fire”
CARGO SMOKE
Smoke has been detected in the cargo (bag-
gage) area
GEAR BAY OVHT TO/LAND
An overheat condition has been detected in the
main landing gear bays
APU FIRE DET FAIL TO/LAND
An APU fire detection system has detected a
failure that will not allow the detection system to
indicate a fire
CARGO SMOKE DET
FAIL
TO/LAND The cargo smoke detection system has failed
L (R) FIRE DET FAIL TO/LAND The engine fire detection system has failed
FIRE SYS FAULT TO/LAND
The fire detection and extinguishing system has
detected a fault
FIREX APU SQUIB
FAIL
TO/LAND
APU fire extinguisher squib on bottle #2 has
failed (NO low pressure indication)
GEAR BAY DET FAIL TO/LAND The gear bay overheat detection has failed
FIRE SYS FAULT TO/LAND The FIREX control unit has detected a fault
FIREX BTL 1 (2) FAULT TO/LAND
The respective bottle squib for the left or right
engine has failed
FIREX BTL 1 (2) LOW TO/LAND The respective bottle pressure is low
FIRE SYS IN TEST
The fire detect test system is conducting the
manually activated system test
FIRE SYS TEST OK
The fire detect test system has passed the sys-
tem test
REV 1