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2. Galley/Cabin Master Switches............................................................................................OFF
3. Boost Pumps ................................................................................................................ALL ON
4. Cross Flow.......................................................................................................................OPEN
5. Battery Switches .......................................................................................................BOTH ON
6. Essential AC Bus ............................................................................... E INV (Manually Select)
7. Essential DC Bus ............................................................................... BATT (Manually Select)
8. Electric Masters Left, Right, Aux Power Switch................................................................OFF
9. ’E’ Batts ...............................................................................................................................OFF
10. If Smoke Stops:
A. FGC 2 Circuit Breaker ............................................................................................. PULL
B. STBY Electrical Power Switch, E INV, TRU.............................................................. ON
C. Symbol Generator 2 and 3 Control Switches ..............................................................ALT
(Top Compact - If Desired)
D. Utility Pump Switch ....................................................................................................OFF
E. Proceed to nearest suitable airport and land.
F. STBY Electrical Power Switch, E INV, TRU.............................................................OFF
(For Approach and Landing)
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 4
EMERGENCY
PROCEDURES
FAA APPROVED 4-35
30 May 2002
11. If Smoke Continues:
A. Electric Masters Left, Right, AUX Power Switch ...........................ON (As Appropriate)
B. ESS AC and DC Buses............................................................................................AUTO
C. Pressurization Control .......................................................................................MANUAL
At Power Distribution Box (PDB):
CAUTION: DO NOT ATTEMPT TO RESET ANY POPPED CIRCUIT BREAKERS.
D. ESS AC and ESS DC Circuit Breakers......................... One (1) at time PULL & RESET
Allow sufficient time (approximately thirty (30) seconds) for smoke to stop between
each PULL and RESET.
CAUTION: PULLING ESS DC BUS PILOT CIRCUIT BREAKER 2 WILL DISABLE
MANUAL CONTROL OF PRESSURIZATION SYSTEM. RESELECT
AUTO MODE IF PULLING THIS CIRCUIT BREAKER STOPS SMOKE.
If Smoke Stops After Any One (1) Circuit Breaker is pulled:
E. Proceed to nearest suitable airport and land.
NOTE: Refer to table in the Quick Reference Handbook (QRH) to assist in determining
inoperative items with a specific Circuit Breaker pulled.
F. Observe Yaw Damper and/or Mach Trim Limits as appropriate.
G. Pressurization Control .............................................................................................AUTO
(If available, ESS AC Pilots PH. A Circuit Breaker)
H. Windshield Heat................................................................OFF two (2) seconds, then ON
I. FGC Circuit Breakers................................................PULL and/or RESET (as necessary)
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 4
EMERGENCY
PROCEDURES
4-36 FAA APPROVED
30 May 2002
12. If Smoke Still Continues:
A. Return Electrical System to Normal Configuration.
B. Windshield Heat................................................................OFF two (2) seconds, then ON
C. FGC Circuit Breakers..................................................PULL and RESET (As Necessary)
D. Check for another source of smoke.
E. Proceed to nearest suitable airport and land.
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 4
EMERGENCY
PROCEDURES
FAA APPROVED 4-37
31 May 2000
4-13-00: FIRE DETECTION SYSTEM
4-13-10: Engine Fire Warning System Malfunction:
Since engine fire warnings (Fire Handle Lights and HP Fuel Cock Lights) are dependent upon
sensing fire/overheat in both loops simultaneously, the possibility exists that a loop could fail
undetected or unannunciated, or that a system fault could develop which causes a signal output
similar to a Fire Warning (i.e., lighted Loop A or B red fire test light), but not both. In these
cases, fire could develop without triggering Fire Warnings, or false fire test light could result,
again without Fire Warning.
The pilot would be alerted to the single activated fire loop by illuminated applicable fire test light
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湾4飞机飞行手册AFM Gulfstream IV AIRPLANE FLIGHT MANUAL 1(100)
