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bus has failed, or input power circuit
breaker is open.
L ALT FAILED BRG light (amber)
illuminated on overhead panel.
Left alternator main bearing has
failed and alternator is operating on
auxiliary bearing.
Quick Reference Handbook
MESSAGES AND ANNUNCIATIONS REVISION 7
Page MB - 22 May 30/02
Caution (Amber) Messages and Annunciations, ctd… OM 04-03-20
Annunciation: Cause(s):
APU ALT FAILED BRG light (amber)
illuminated on overhead panel.
APU alternator main bearing has
failed and alternator is operating on
auxiliary bearing.
R ALT FAILED BRG light (amber)
illuminated on overhead panel.
Right alternator main bearing has
failed and alternator is operating on
auxiliary bearing.
L/R ENG IDLE light (amber)
illuminated on windshield center
post.
Engine idle is in low range when it
should be scheduled to high range.
OR:
Engine idle is in high range when it
should be scheduled to low range.
See Approach Idle System Failure,
page EC-15.
Amber chevron illuminated on
pilot’s/copilot’s AOA indexer.
AOA for approach and landing is too
low.
AP OFF light (amber) illuminated on
Pilot’s / Copilot’s Master Warning
and Caution Lights Panel.
Autopilot disconnected.
AT OFF light (amber) illuminated on
Pilot’s / Copilot’s Master Warning
and Caution Lights Panel.
Autothrottle disconnected.
LOW FUEL light(s) (amber)
illuminated on standby fuel quantity
indicator.
Fuel level in respective hopper is
below approximately 650 lb (295 kg).
APU LOAD light (amber) illuminated
above DU 2 or 5.
(SPZ-8400 equipped)
APU electrical load for operations
above 30,000 ft. not within limits.
ELWS CONFIG light (amber)
illuminated above DU 2 or 5.
(SPZ-8400 equipped)
APU electrical power improperly
configured for operations above
30,000 ft.
ELWS FAIL light (amber) illuminated
above DU 2 or 5.
(SPZ-8400 equipped)
APU electrical power unreliable for
operations above 30,000 ft.
N COOL VALVE OPEN light (amber)
illuminated above DU 2 or 5.
Nose compartment cooling valve is
open.
HORN SILENCE light (amber)
illuminated on Landing Gear Control
Panel.
Airplane is below 1200 ft. AGL (radio
altitude), all three landing gear not
down and locked, flaps less than 22°,
and power lever is retarded below
70%.
Quick Reference Handbook
REVISION 7 MESSAGES AND ANNUNCIATIONS
May 30/02 Page MB - 23
Caution (Amber) Messages and Annunciations, ctd… OM 04-03-20
Annunciation: Cause(s):
Amber light illuminated above
differential pressure indicator.
Cabin differential pressure has
reached 9.6 psi.
Amber light illuminated above APU
EGT indicator.
APU is at 100% speed and EGT has
exceeded 688°.
Amber light illuminated above APU
RPM indicator.
APU RPM has exceeded 104%.
Quick Reference Handbook
MESSAGES AND ANNUNCIATIONS REVISION 7
Page MB - 24 May 30/02
Notes
Quick Reference Handbook
REVISION 7 MESSAGES AND ANNUNCIATIONS
May 30/02 Page MC - 1
Advisory (Blue) Messages and Annunciations Index
Message Page
AC EXT POWER .........................(DC EXT POWER Also)...........MC-4
AP CTLR SW STUCK....................................................................MC-4
AP ENGAGE INHIBIT ....................................................................MC-4
APU ALT OFF................................................................................MC-4
APU EXCEEDANCE......................................................................MC-5
AT ENGAGE INHIBIT ....................................................................MC-5
AT 1-2 FAIL....................................................................................MC-5
AT NOT IN HOLD ..........................................................................MC-5
BC 1-2-3 TEST FAIL ......................................................................MC-6
BRAKE MAINT REQ’D ................(Brake-By-Wire Airplanes) .......MC-6
BRAKE MAINT REQ’D ................(HMAB Airplanes) ....................MC-6
BUS CTLR 1-2-3 FL.......................................................................MC-7
CALL ..............................................................................................MC-7
CDU 1-2 FAIL.................................................................................MC-7
CHECKLIST MISMATCH...............................................................MC-7
CMB HYD HOT ..............................................................................MC-7
　
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