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FGC.
Determine cause of FGC fault.
SERVICE DOORS One or more of service
doors is open.
Close service doors.
SG 1-2-3 FAIL Indicated symbol generator
has failed.
Switch appropriate symbol generator to
"ALT" and momentarily select a
different mode on the navigation display.
SG 1-2-3 HOT Symbol generator hot. Check avionic rack ventilation. Select
alternate symbol generator and pull hot
SG CB.
SPD BRAKE EXTNDED Speed brakes are extended. Retract speed brakes.
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 3
ABNORMAL
PROCEDURES
FAA APPROVED 3B-15
29 January 2002
BLUE ADVISORY MESSAGES
CAS INDICATION CAUSE CORRECTIVE ACTION
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.
2. Verify transponder and altitude
reporting is selected ON.
TERRAIN NOT AVAIL Terrain awareness is not
available.
1. Check CBs:
- EGPWS AC; CP, D-10
- EGPWS DC; CP, E-10
2. Verify at least one (1) radio altimeter
is available.
TONE GEN FAIL
or
TONE GEN 1-2 FAIL
(SPZ 8400 equipped)
Aural warning tone
generator has failed.
Check Circuit Breakers. Reset if
required. Proceed with flight. No aural
tones will be available.
VHF COMM 1-2-3 FL Self explanatory. Check status of VHF radio.
VNAV TRACK
CHANGE
One (1) minute prior to
vertical navigation track
change.
No action.
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 3
ABNORMAL
PROCEDURES
3B-16 FAA APPROVED
29 January 2002
BLUE ADVISORY MESSAGES
CAS INDICATION CAUSE CORRECTIVE 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 CBs:
- 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 CBs:
- EGPWS AC; CP, D-10
- EGPWS DC; CP, E-10
2. Verify at least one (1) radio altimeter
is available.
L-R WING A/I Wing anti-ice On. Turn OFF wing anti-ice after departing
icing conditions.
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 4
EMERGENCY
PROCEDURES
FAA APPROVED 4-i
31 May 2000
TABLE OF CONTENTS
SUBJECT: SECTION: PAGE:
Emergency Procedures................................................................ 4-00-00 ...................4-1
General Guidance ..................................................................... 4-00-10 ...................4-1
Brakes System.............................................................................. 4-05-00 ...................4-2
Emergency Brakes (Brake-By-Wire) ........................................ 4-05-10 ...................4-2
Emergency Brakes (HMAB)..................................................... 4-05-20 ...................4-3
Electrical Power System.............................................................. 4-07-00 ...................4-5
Alternator/Converter Failure - Dual ......................................... 4-07-10 ...................4-5
Essential DC Bus Power Failure............................................... 4-07-20 ..................4-10
Electrical System - Battery Only Operation.............................. 4-07-30 ..................4-12
Engine Failure.............................................................................. 4-09-00 ..................4-13
Engine Failure........................................................................... 4-09-10 ..................4-13
Engine Failure During Takeoff Below V1 Speed ..................... 4-09-20 ..................4-14
Engine Failure During Takeoff Above V1 Speed ..................... 4-09-30 ..................4-15
Dual Engine Flameout .............................................................. 4-09-40 ..................4-16
Dual Engine Out Approach and Landing Procedure ................ 4-09-50 ..................4-19
　
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