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2. Select alternate symbol
generator and pull hot SG CB:
(SYM GEN #1: CP, K-3; SYM
GEN #2, CP, L-3; SYM GEN
#3, CP, M-3.)
SPD BRAKE
EXTNDED
Speed brakes
are extended.
Retract speed brakes.
SPD BRAKE
SWITCH
FWC and FGC
disagree on
position of
speed brakes.
Check adjustment of speed brake
extended signal to FWC and
FGC at next maintenance
opportunity.
T&L >80% FULL
(Added by ASC 415
for SPZ 8000
airplanes.)
FWC memory
is greater than
80% full.
Download and erase FWC
memory at next convenient
maintenance period.
TCAS FAIL Traffic Alert and
Collision
Avoidance
System (TCAS)
has failed.
1. Check TCAS circuit breaker
(TCAS: CP, D-11.)
2. Verify transponder and altitude
reporting is selected ON.
TERRAIN NOT
AVAIL
Terrain
awareness is
not available.
1. Check circuit breakers:
EGPWS AC: CP, D-10
EGPWS DC: CP, E-10
2. Verify at least one (1) radio
altimeter is available.
Quick Reference Handbook
REVISION 7 MESSAGES AND ANNUNCIATIONS
May 30/02 Page MC - 15
Advisory (Blue) Messages and Annunciations, ctd… AFM 3B
Message: Cause(s): Corrective Action:
TONE GEN FAIL
OR:
TONE GEN 1-2
FAIL
(SPZ 8400
equipped)
Aural warning
tone generator
has failed.
1.Check circuit breakers.
2.Reset if required.
3. Proceed with flight.
4.No aural tones will be
available.
VHF COMM 1-2-3
FL
Self explanatory. Check status of VHF radio.
VNAV TRACK
CHANGE
One minute prior
to vertical
navigation track
change.
No action.
VOICE REC
FAIL
Self
explanatory.
No action.
VOR COURSE Autopilot has
sensed being
over station
while coupled
to LNAV
(VOR/TCN).
If desired, course selector may
now be changed more than 3°
without dropping LNAV
(VOR/TCN) mode.
WS FAIL Windshear
function of
GPWS has
failed.
1. Check circuit breakers:
EGPWS AC: CP, D-10
EGPWS DC: CP, E-10
2. Verify at least one (1) radio
altimeter is available.
WS
UNAVAILABLE
Windshear
function of
GPWS not
available.
1. Check circuit breakers:
EGPWS AC: CP, D-10
EGPWS DC: CP, E-10
2. Verify at least one (1) radio
altimeter is available.
WING A / I, L-R Wing anti-ice
On.
Turn OFF wing anti-ice after
departing icing conditions.
Quick Reference Handbook
MESSAGES AND ANNUNCIATIONS REVISION 7
Page MC - 16 May 30/02
Advisory (Blue) Messages and Annunciations, ctd… OM 04-04-20
Annunciation: Cause(s):
"Single Chime" aural tone sounds. A new ADVISORY (blue) message is
displayed on CAS. The new
message will be displayed flashing
on the top of the ADVISORY
messages stack. The aural tone will
then automatically cease and
message will automatically revert to
steady display.
"Cricket" aural tone sounds. Airplane Overspeed
"Beep" aural tone sounds. Altitude Alert
LEFT/RIGHT WING WARM light
(blue) illuminated on overhead panel.
Wing anti-ice plenum in wing leading
edges has reached minimum operating
temperature of 100° F (38° C).
EXT BATT SW light (blue)
illuminated on overhead panel.
External battery switch on.
AC EXT PWR light (blue) illuminated
on overhead panel.
AC external power applied.
DC EXT PWR light (blue) illuminated
on overhead panel.
DC external power applied.
LEFT/RIGHT FRONT/SIDE
WINDOW light (green) illuminated
on overhead panel.
Windshield heat operating.
REV ARM light (green) illuminated
above Display Unit (DU) 2 or 5.
Parameters satisfied for thrust
reverser deployment.
LH RR FAN FAIL light (blue)
illuminated on copilot's side panel.
(1)
Left hand radio rack cooling fan has
failed.
RH RR FAN FAIL light (blue)
illuminated on copilot's side panel.
(1)
Right hand radio rack cooling fan has
failed.
RH RR FAN AUTO light (blue)
illuminated on copilot's side panel.
(1)
Right hand radio rack cooling fan
operating automatically.
RH RR FAN MAN ON light (blue)
illuminated on copilot's side panel.
(1)
Right hand radio rack cooling fan
operating manually.
SPEED BRAKE handle illuminated
(pale blue).
SPEED BRAKE handle not in
RETRACT detent.
(1) SN 1156 and subs.
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湾流4快速检查单QRH GULFSTREAM IV QUICK REFERENCE HANDBOOK 2(72)
