Amber Caution Messages - Honeywell PRIMUS 1000 Pilot's Manual

If there are amber messages already on the CAS display when a new
amber message becomes active, the new message is put at the top of
the amber message stack. If the existing amber or cyan messages are
scrolled of the display, the amber and cyan message stacks are brought
back on the CAS display with the new message displayed at the top of
the amber stack. Messages are removed from the CAS display when
the condition that caused the message is remedied. Table 5--19 list the
caution messages.
Amber messages with a D are not inhibited during takeoff and landing.
115 VAC BUS OFF
ACCESS DOORS OPEN
AHRS 1 OVERHEAT
AHRS 2 OVERHEAT
A/ICE SWITCH OFF
AIL SYS 1 INOP
AIL SYS 2 INOP
AP AIL MISTRIM
AP ELEV MISTRIM
APU BLD VLV FAIL
APU CNTOR CLSD
APU EXTBTL INOP
APU FAIL
APU FIREDET FAIL
APU FUEL LO PRESS
APU FUEL SOV INOP
APU GEN OFF BUS
APU GEN OVLD
APU OIL HI TEMP
APU OIL LO PRESS
AOA 1 HEAT INOP
AOA 2 HEAT INOP
AURAL WARN FAIL
AUTO TRIM FAIL
AUTOPILOT FAIL
BAGGAGE DOOR OPN
BATT 1 OFF BUS
BATT 2 OFF BUS
BKUP BATT OFF BUS
BLD 1 TEMP
BLD 1 VLV FAIL
A28--1146--112--00
PRIMUSr1000 Integrated Avionics System
BLD 2 TEMP
BLD 2 VLV FAIL
BRAKE OVERHEAT D
BRAKE DEGRADED
BRK INBD INOP
BRK OUTBD INOP
CHECK PFD 1
CHECK PFD 2
CROSS BLD FAIL
CROSS BLD SW OFF
DAU1 A FAIL
DAU2 A FAIL
DAU 1 ENG MISCMP
DAU 1 SYS MISCMP
DAU 1 WRN MISCMP
DAU 2 ENG MISCMP
DAU 2 SYS MISCMP
DAU 2 WRN MISCMP
DC BUS 1 OFF
DC BUS 2 OFF
DFDR FAIL
E1 A/ICE FAIL
ELEKBAY OVTEMP
EMERG LT NOT ARMD
EMERG EXIT OPN
EMRG BRK LO PRES
ENG 1 REV FAIL
ENG 1 TLA FAIL
ENG 2 REV FAIL
ENG 2 TLA FAIL
ENG NO TO DATA

Amber Caution Messages

Table 5--19 (cont)
Engine Instrument and Crew Alerting System (EICAS)
5-25