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RED WARNING MESSAGES
CAS INDICATION SWLP INDICATION CAUSE CORRECTIVE ACTION
ENGINE
EXCEEDANCE
(SPZ 8400 equipped)
(added by ASC 415
for SPZ 8000
airplanes)
NONE LP, HP, or TGT above
limit.
Retard throttle(s) to
achieve power setting
within limits. Shut down
engine if exceedance
persists with throttle at
idle.
ENG FIRE LOOP
ALRT
FIRE DET LOOP Engine fire loop
senses fire.
If Fire Handle and HP
cock are illuminated, fire
warning is valid - Execute
Engine Fire Procedure,
Section 4.
If Fire Handle and HP
cock are not illuminated,
check Fire Detection Panel
- perform fire test. If test
good, isolate faulty loop.
Test bad - execute
ENGINE FIRE Procedure,
Section 4.
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 4
EMERGENCY
PROCEDURES
FAA APPROVED 4A-5
31 May 2000
RED WARNING MESSAGES
CAS INDICATION SWLP INDICATION CAUSE CORRECTIVE ACTION
L-R ENGINE HOT L ENGINE HOT
R ENGINE HOT
Engine cooling air
temperature above
860°F (460°C).
See procedure in Section
4.
FLAME DETECT FLAME DETECT Flame in area
annunciated by
illuminated
annunciation.
Refer to Emergency
Procedures Section 4, for
area in which flame is
detected.
L-R FUEL FILTER L FUEL FILTER
R FUEL FILTER
Fuel filter clogging. Retard power lever to 75%
HP. Check that fuel
temperature increased to
above +5°, and hold this
condition for ten (10)
seconds before restoring
engine power. Shut down
engine if operation
becomes erratic.
NOTE: If fault shows on
both engines, apply above
procedure to only one
engine at a time. Land as
soon as possible.
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 4
EMERGENCY
PROCEDURES
4A-6 FAA APPROVED
11 October 2001
RED WARNING MESSAGES
CAS INDICATION SWLP INDICATION CAUSE CORRECTIVE ACTION
L-R FUEL PRESS
LOW
L FUEL PRESS
R FUEL PRESS
Fuel pressure at inlet
to high pressure fuel
pump is less than 15
psi or both fuel boost
pumps on one side
have been turned off
with crossflow valve
CLOSED.
Check that boost pumps
are ON and functioning.
Check crossflow valve
position. Check for erratic
fuel flow indication. Shut
down engine if operation
becomes erratic.
GND SPOILER GND SPOILER Failure of ground.
spoiler component or
deployed ground
spoiler panel.
Immediately select ground
spoiler Arming switch
OFF. See Section 4-15-
50: Ground Spoiler
Failure.
FWD LAV SMOKE
DETECT
(SPZ 8400 equipped)
NONE Smoke detected in
FWD LAV area or
Radio Rack Area.
Refer to Section 4, Smoke
in Baggage Compartment,
Aft Galley or Lavatory or
Right Hand Avionics Bay
procedure.
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 4
EMERGENCY
PROCEDURES
FAA APPROVED 4A-7
31 May 2000
RED WARNING MESSAGES
CAS INDICATION SWLP INDICATION CAUSE CORRECTIVE ACTION
L-R OIL PRESS
LOW
L OIL PRESS
R OIL PRESS
Indicated oil pressure
below 16 psi.
Check oil pressure reading.
Minimum oil pressure 16
psi below 76% HP RPM.
Shut down engine if
pressure abnormally low.
L-R PYLON HOT L PYLON HOT
R PYLON HOT
Pylon temperature is
above 325°F (163°C).
Appropriate bleed air
switch OFF. Check
isolation valve closed.
Descend to 41,000 ft.
Monitor message. Prepare
for possible engine
shutdown. If problem
persists, land as soon as
possible.
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 4
EMERGENCY
PROCEDURES
4A-8 FAA APPROVED
31 May 2001
RED WARNING MESSAGES
CAS INDICATION SWLP INDICATION CAUSE CORRECTIVE ACTION
RADIO RACK
SMOKE
(added by ASC 415
for SPZ 8000/8400
airplanes and SN 1390
and sub)
SMOKE DETECT Smoke detected in
Radio Rack Area.
Refer to Emergency
Procedures Section 4, for
area in which smoke is
detected.
L-R REV UNLOCK REV UNLOCKED Thrust Reverser has
become unlocked.
Ensure thrust reverse lever
is stowed and retard
affected engine to idle.
Reduce airspeed to less
than 200 KCAS and
depress T/REV EMERG
STOW switch. See
procedure in Section 4.
CAUTION: DO NOT ATTEMPT TO DEPLOY AND RESTOW
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湾4飞机飞行手册AFM Gulfstream IV AIRPLANE FLIGHT MANUAL 1(112)
