Honeywell PRIMUS 1000 - Page 165

PRIMUSr 1000 Integrated Avionics System
A28--1146--112--00
Engine Instrument and Crew Alerting System (EICAS)
5-26
E1 ATS SOV OPN
E1 CTL A FAIL
E1 CTL B FAIL
E1 EXTBTL A INOP
E1 EXTBTL B INOP
E1 FIREDET FAIL
E1 FUEL LO PRESS
E1 FUEL LO TEMP
E1 FUEL SOV INOP
E2 A/I FAIL
E2 ATS SOV OPN
E2 CTL A FAIL
E2 CTL B FAIL
E2 EXTBTL A INOP
E2 EXTBTL B INOP
E2 FIREDET FAIL
E2 FUEL LO PRESS
E2 FUEL LO TEMP
E2 FUEL SOV INOP
ELEC EMERG ABNORM
ENG REF A/I DISAG
ESS BUS 1 OFF
ESS BUS 2 OFF
FLAP FAIL
FUELING DOOR OPN
FUEL IMBALANCE
FUEL TANK LO TEMP
FUEL XFEED FAIL
GEN 1 OFF BUS
GEN 1 OVLD
GEN 2 OFF BUS
GEN 2 OVLD
GEN 3 OFF BUS
GEN 3 OVLD
GEN 4 OFF BUS
GEN 4 OVLD
GPWS INOP D
HS VLV 1 FAIL
HS VLV 2 FAIL
HYD SYS 1 FAIL
HYD SYS 1 OVHT
HYD SYS 2 FAIL
HYD SYS 2 OVHT
IC 1 OVERHEAT
IC 1 WOW INOP
IC 2 OVERHEAT
IC 2 WOW INOP
IC BUS FAIL
ICE DET 1 FAIL
ICE DET 2 FAIL
ICE DETECTORS FAIL
ITT 1 LIMIT FAIL
ITT 2 LIMIT FAIL
LG AIR/GND FAIL D
NO ICE A/ICE ON
OXYGEN LO PRESS
OVER WG ICE DET
OVER WG ICE INOP
PACK 1 OVHT
PACK 1 OVLD
PACK 1 VLV FAIL
PACK 2 OVHT
PACK 2 OVLD
PACK 2 VLV FAIL
PITOT 1 INOP
PITOT 2 INOP
PITOT 3 INOP
PRESN AUTO FAIL
RAM AIR VLV FAIL
RUD HDOV PROT FAIL
RUDDER OVERBOOST
RUDDER SYS1 INOP
RUDDER SYS2 INOP
SHED BUS 1 OFF
SHED BUS 2 OFF
SPBK LVR DISAGREE
SPOILER FAIL
SPS ADVANCED D
STAB A/ICE FAIL
STEER INOP
STICK PUSHER FAIL D
TAT 1 HEAT INOP
TAT 2 HEAT INOP
WG 1 A/ICE FAIL
WG 2 A/ICE FAIL
WG A/ICE ASYMETRY
WINDSHEAR INOP D
W/S 1 HEAT FAIL
W/S 2 HEAT FAIL
YAW DAMPER FAIL
Amber Caution Messages
Table 5--19