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resolved weight-off wheels.
DISP CTLR 1-2
FAIL
A display
controller has
failed.
No action. Use remaining display
controller where applicable.
DU 1-2-3-4-5-6
HOT
DU hot (266°F
[130°C]).
1. Select DU OFF.
2. If message clears, select DU
ON.
3. If message returns, select DU
OFF and leave off for
remainder of flight.
E BATT 1-2-3*-4*
DISCH
(* if installed)
Emergency
battery is
discharging.
1. Ensure E BATT is not on.
2. If battery is not on, pull and
reset circuit breaker to attempt
to clear message (AFT EMER
BATT: P, I-13; FWD EMER
BATT: P, H-13.)
3. If message does not clear, no
further action is required.
4. Breaker should be left closed
and system rearmed as
required.
E BATT 1-2-3*-4*
FAIL
(* if installed)
Self
explanatory.
Turn off emergency battery.
ENGINE COWL
OPEN
Engine cowl
door is open.
Close door.
ENGINE
EXCEEDANCE
(Deleted by ASC 415
for SPZ 8000
airplanes.)
OR:
EXCEEDANCE
RECORD
(SPZ 8400 equipped)
Fault warning
computer has
recorded an
exceedance.
1. Check engine instruments.
2. Reduce thrust by appropriate
engine(s) within limits.
3. May be caused by engine fire.
4. Take appropriate action.
5. Recording may be viewed by
selecting EXCEEDANCES on
SYSTEMS menu of display
controller.
Quick Reference Handbook
MESSAGES AND ANNUNCIATIONS REVISION 7
Page MC - 10 May 30/02
Advisory (Blue) Messages and Annunciations, ctd… AFM 3B
Message: Cause(s): Corrective Action:
EPR 1 - DADC 2
EPR 2 - DADC 1
DADC
malfunction has
caused
remaining
DADC to
supply
information to
both EPR
systems.
Verify status of DADCs.
EXT BATT
SWITCH ON
External battery
switch on.
Turn external battery switch OFF.
FGC 1-2 MASTER A shift in
controlling FGC
has occurred:
indicated FGC
has taken over.
Message times
out
automatically.
1. Check SENSOR page.
2. Shift back to other FGC, if
desired, or leave as is.
FGC NOT USING
IRS 1-2
IRS data has
been rejected
by FGC due to
unflagged
miscompare
between IRS
1/2 or flagged
IRS failure.
1. Check IRS condition / status on
FMS IRS status page.
2. System performance is same
with 1 or 2 IRS sources.
FGC SYSTEM
TEST
Maintenance
switch is on.
Turn off maintenance switch
located in each avionics rack.
FLT HYD HOT Hydraulic
system fluid
temperature
above 220° F
(104° C).
1. If flight system is hot and utility
pressure is required, utility
hydraulic pump switch must be
set to ON.
2. If utility system is not required,
turn utility pump OFF.
Quick Reference Handbook
REVISION 7 MESSAGES AND ANNUNCIATIONS
May 30/02 Page MC - 11
Advisory (Blue) Messages and Annunciations, ctd… AFM 3B
Message: Cause(s): Corrective Action:
FLIGHT REC FAIL Flight recorder
has failed. It is
normal for this
message to be
illuminated until
an engine is
started and 10
psi oil pressure
is attained.
1. Check circuit breakers (CP, C-
7, C-8, C-9.)
2. Pull and reset if necessary.
3. Check FDR Ground
Maintenance Override Switch
in right hand avionics bay to be
in AUTO.
4. Check for FDAU and / or DFDR
fail annunciators and record for
maintenance.
FUEL INT TANK
OPEN
Fuel intertank
valve is open.
Select fuel intertank OFF.
FUEL XFLOW
OPEN
Fuel crossflow
is open.
Select fuel crossflow OFF.
FWC 1-2 FAIL Fault warning
computer has
failed.
Select other FWC.
FWD EXT SW PNL
OPN
Forward
external switch
panel door is
open.
Close door.
FWD LAV SVC DR
OPN
Forward
lavatory service
door is open.
Close door.
GND SPOILER
UNARM
Ground spoilers
not armed.
Check switch; cycle to ARMED.
GPWS FAIL Ground
Proximity
Warning
System
(GPWS) has
failed.
1. Check GPWS circuit breaker:
EGPWS AC: CP, D-10
EGPWS DC: CP, E-10
2. Verify at least one radio
altimeter is available.
IRS 1-2 FAIL Indicated IRS
has failed.
Verify failure on MSU panel and,
if being used, select another
　
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