Honeywell PRIMUS 1000 - Caution Messages (Amber); Elec Ess Xfr Fail; No Takeoff Config; Red Warning Messages

PRIMUSr 1000 Integrated Avionics System
A28--1146--112--00
Engine Instrument and Crew Alerting System (EICAS)
5-24
APU FIRE D
AUTOPILOT FAIL
BAGG SMOKE
BATT 1 OVTEMP D
BATT 2 OVTEMP D
BLD 1 LEAK
BLD 2 LEAK
BLD 1 OVTEMP
BLD 2 OVTEMP
BLD APU LEAK
E1 ATTCS NO MRGN
E2 ATTCS NO MRGN
E1 LOW N1
E2 LOW N1
E1 OIL LOW PRESS
E2 OIL LOW PRESS
ELEC ESS XFR FAIL D
ENG 1 FIRE D
ENG 2 FIRE D
ENG ATTCS FAIL
FUEL 1 LO LEVEL
FUEL 2 LO LEVEL
GPWS D
ICE COND -- A/I INOP D
LAV SMOKE
LG/LEVER DISAGREE D
MAIN DOOR OPN
NO TAKEOFF CONFIG
PIT TRIM 1 INOP
PIT TRIM 2 INOP
SPS 1 INOP D
SPS 2 INOP D
SERVICE DOOR OPN D
NOTE: Red messages with a D are not inhibited during takeoff and landing.
Red Warning Messages
Table 5--18
D NO TAKEOFF CONFIG -- This message is displayed when the
aircraft is on the ground, either engine thrust lever isat greater than
60°, and any of the following conditions exist:
- The parking brake is on
- Ground spoilers are deployed
- Pitch trim is greater than --4° or less than --8°
- Flaps are not at either 9° or 22°.
D ELEC ESS XFR FAIL -- The following combination triggers this
message:
- The L air/ground switch indicates airborne and
- Either L or K essential bus contact indicates open or L or R dc
bus indicates off and
- Generators 1 through 4 line contacts indicate open and
- APU generator line contact indicates open.
CAUTION MESSAGES (AMBER)
Whenanambermessagebecomesactive,thefollowingindicationsare
given:
D Amber message displayed flashing on the CAS display
D Ambercautionannunciatoronthewarning/cautionannunciatorislit.
When the warning/caution annunciator/pushbutton is selected on the
master warning panel, the amber annunciator is extinguished and the
amber message is displayed steadily on the CAS display.