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IGNITION A/B Ignition systems A and B are on during
continuous ignition conditions.
APU
APU SOV CLSD
APU fuel feed and negative-g shut off
valves are confirmed closed after APU
fire push switch is pushed, during an
APU fire condition.
BLEED
DUCT TEST OK 10th and 14th stages, bleed leak
detection test successful.
LOOP A (B) TEST OK Duct overheat loop circuit test
successful.
COMMUNICATIONS
SELCAL HF1 (2) SELCAL has been activated by
ground station on the respective high
frequency radio.
DOORS
DOOR CLOSED PAX door latches locked, handle
stowed and airplane is on the ground.
EICAS
FDR EVENT Flight data recorder event marker.
FIRE PROTECTION
APU SQUIB 1 (2) OK APU firex squib 1 (2) test successful.
L (R) ENG SQUIB 1 (2) OK L (R) engine firex squib 1 (2) test
successful.
ADVISORY-1
REV 66, Feb 01/07
QUICK REFERENCE HANDBOOK
PSP 604-15 ADVISORY MESSAGES
FLIGHT CONTROLS
AILERON MON OK Aileron PCU comparator monitor self
test successful.
T/O CONFIG OK Engines running with flaps, flight
spoilers, parking brake and stabilizer
trim correctly set for take-off.
FLIGHT INSTRUMENTS
IRS 3 ALIGNING
(if installed)
IRS 3 (if installed) is in align mode.
Do not taxi.
FUEL
L (R) ENG SOV CLSD L (R) engine SOV closed, after
respective engine fire push switch is
pushed.
L (R) FUEL PUMP ON L (R) fuel pump on, with sufficient
outlet fuel pressure.
HYDRAULIC
HYD SOV 1 (2) CLSD Hydraulic SOV 1 (2) confirmed
closed, after respective engine fire
push switch is pushed.
ICE
COWL A/ICE ON Both cowl anti-ice on with sufficient
heat and with the engines running.
L (R) COWL A/ICE ON L (R) cowl anti-ice on with sufficient
heat and with respective engine
running.
WING A/ICE OK Wing anti-ice test successful.
WING A/ICE ON Wing anti-ice is on and sufficient heat
is being supplied to the wing.
WING/COWL A/ICE ON Both cowl and wing anti-ice are on
with the engines running and
sufficient heat is being supplied
respectively.
L (R) WINDOW HEAT OK L (R) window heat test successful.
L (R) WSHLD HEAT OK L (R) windshield heat test successful.
ICE Icing is detected, but wing and cowl
anti-ice are both on.
ADVISORY-2
REV 66, Feb 01/07
QUICK REFERENCE HANDBOOK
PSP 604-15 ADVISORY MESSAGES
LANDING GEAR
PARKING BRAKE ON Parking brake set with one or both
engines less than 70% N1.
A/SKID IN TEST Anti-skid system undergoing self test
(with the parking brake off).
ADVISORY-3
REV 66, Feb 01/07
QUICK REFERENCE HANDBOOK
PSP 604-15 ADVISORY MESSAGES
ADVISORY-4
REV 66, Feb 01/07
QUICK REFERENCE HANDBOOK
PSP 604-15 ADVISORY MESSAGES
THIS PAGE INTENTIONALLY LEFT BLANK
The following messages (white) annunciate conditions that require
time-available corrective action.
AUTOMATIC FLIGHT CONTROLS (AFCS)
AFCS 1 (2) INOP Respective autopilot system is
inoperative.
FD 1 (2) FAIL Respective flight director is
inoperative.
IAPS DEGRADED Integrated avionics processing system
(IAPS) degraded, failure of any of
IAPS busses on the ground.
IAPS OVERTEMP IAPS overtemperature.
VSPD/ALT REFS INDEP Pilot’s and copilot’s V speed selections
are not synchronized.
YD 1 (2) INOP Respective yaw damper is not
engaged or is failed; other channel
engaged / not failed.
BLEED
CKPT HEAT FAN FAIL Cockpit heat fan failure.
DISPLAY COOL FAIL EFIS or EICAS display fan failure.
EXHAUST FAN FAIL Exhaust (avionics cooling) fan failure.
DOORS
EXTERNAL DOOR OPEN All external doors not closed and
latched.
ELECTRICAL
AC ESS ALTN AC essential bus is powered by AC
bus 2.
AC UTIL 1 (2) OFF AC utility bus 1 (2) is not powered.
APU BATT CHGR FAIL APU battery charger failure or APU
battery is not charging.
ESS TRU 1 (2) FAIL Respective essential transformer
rectifier unit (TRU) output is less than
18VDC and AC essential bus is not
failed.
MAIN BATT CHGR FAIL Main battery charger failure or main
battery is not charging.
STATUS-1
REV 66, Feb 01/07
QUICK REFERENCE HANDBOOK
PSP 604-15 STATUS MESSAGES
ENGINE
DCU 1 (2) (3*) APR FAIL
(* - if installed)
APR relay did not energize during the
test.
L (R) ENG ECU FAIL APR relay has energized, but APR
circuit not triggered.
FLIGHT CONTROLS
STAB CH 1 (2) INOP Respective channel not engaged or
failed; other channel engaged / not
failed.
FLAPS MOTOR OVHT One or both of the flap motors
　
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