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PROCEDURES
4-70 FAA APPROVED
31 May 2000
4-25-00: WINDSHIELDS/DOOR SYSTEMS
4-25-10: Windshield Failure:
If windshield heat failure is detected, cycle the windshield heat control OFF, then ON. If
windshield heat can not be regained, flight may be continued, but flight into icing conditions
should be avoided. If failure involves a front window, pull appropriate circuit breaker located on
C/P aft C.B. Panel under ANTI-ICE. (L FRONT POWER, R FRONT POWER, L. SIDE
WSHLD, R. SIDE WSHLD)
Windshield crack(s):
1. Upon detection of a crack in outer heating/protective windshield ply, immediately turn
windshield heat OFF on affected panel by pulling the appropriate circuit breaker located on
C/P aft C.B. Panel under ANTI-ICE and observe icing restrictions. (L FRONT POWER, R
FRONT POWER, L. SIDE WSHLD, R. SIDE WSHLD)
2. Upon detection of a crack in either main structural windshield ply, a reduction of cabin
pressure differential to 7.5 psi is recommended for remainder of flight.
3. Maintain current airspeed/mach or slower for remainder of flight.
4. Refer to the Configuration Deviation List - Appendix B for subsequent takeoff
considerations.
WARNING: IF CRACKING IS TO THE INNER GLASS PLY, IT IS RECOMMENDED
THAT THE PILOT ADJACENT TO THE CRACK AREA WEAR EYE
PROTECTION SUCH AS SMOKE GOGGLES.
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 4
EMERGENCY
PROCEDURES
FAA APPROVED 4A-1
31 May 2000
RED WARNING MESSAGES
CAS INDICATION SWLP INDICATION CAUSE CORRECTIVE ACTION
ACFT
CONFIGURATION
ACFT CONFIG Check Flap, Speed
Brake, and Landing
Gear lever positions.
Correct configuration.
AFT BAG SMOKE
(SPZ 8400 equipped)
SMOKE DETECT Smoke detected in aft
baggage compartment.
See procedure in Section
4.
AFT EQUIP HOT AFT EQUIP HOT Aft equipment area
temperature above
200°F (93°C).
Possibility exists that
high pressure duct has
blown or that fire is in
progress.
Identify faulty side by
checking for high TGT,
high fuel flow, low EPR
or low (abnormal) bleed
pressure. Shut off faulty
side bleed pressure switch.
Check isolation valve
closed. Descend to 41,000
ft. Monitor message. See
procedure in Section 4.
Land as soon as possible.
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 4
EMERGENCY
PROCEDURES
4A-2 FAA APPROVED
11 October 2001
RED WARNING MESSAGES
CAS INDICATION SWLP INDICATION CAUSE CORRECTIVE ACTION
APU FIRE APU FIRE APU Fire 1. APU Overspeed Test -
PRESS
2. APU Master – OFF
3. APU Fire Extinguisher
–PRESS
4. APU Fire Test - PRESS
See Section 4-12-30: APU
Fire.
APU LOAD
(SPZ 8400 equipped)
NONE APU Electrical Load
for operations above
30,000 ft not in limits.
Select CABIN MASTER
OFF.
CABIN DFRN-9.8 NONE Cabin differential
press approaching
upper limit (9.8).
Raise cabin altitude.
Increase rate of climb of
cabin, if required.
CABIN PRESSURE
LOW
CAB PRESS LOW Cabin altitude has
climbed above limits
(9250 ft. ±750 ft).
Check cabin pressure
indicator and controls.
Descend as necessary. Use
oxygen, as appropriate.
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 4
EMERGENCY
PROCEDURES
FAA APPROVED 4A-3
31 May 2000
RED WARNING MESSAGES
CAS INDICATION SWLP INDICATION CAUSE CORRECTIVE ACTION
CHECK PFD
CHECK PFD 1-2
(SPZ 8400 equipped)
NONE Hazardously
misleading
information on both
PFD’s.
Check pitch, roll, airspeed
and altitude on both PFD’s
to verify information is
correct.
DAU 1-2 MISCMPMSG
NONE Miscompare between
data channels, of a
serious nature.
Attempt to identify faulty
channel then switch to
sensor page and select
good channel of respective
DAU.
DOOR BAGGAGE
(deleted by ASC 415
changed to Amber
Message for SPZ
8000/8400 airplanes
and 1390 and sub)
DOOR MAIN
CABIN DOORS Main or baggage door
not locked.
Reduce cabin pressure
differential. Check locking
handles for security.
Exercise care when in
vicinity of doors. If main
door does not appear
secure, land as soon as
possible. If doors appear
secure, continue flight.
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 4
EMERGENCY
PROCEDURES
4A-4 FAA APPROVED
31 May 2000
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湾4飞机飞行手册AFM Gulfstream IV AIRPLANE FLIGHT MANUAL 1(111)
