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D. UTILITY PUMP......................................................................................OFF
E. Airplane .....PROCEED TO NEAREST SUITABLE AIRPORT AND LAND
F. STANDBY ELECTRICAL POWER STBY ELEC, E INVERT and TRU......
OFF FOR APPROACH AND LANDING
IF SMOKE CONTINUES:
11. Airplane Systems....................................................CONFIGURE AS FOLLOWS
A. ELECTRIC MASTER LEFT PWR, RIGHT PWR and AUX PWR ..ON (AS
APPROPRIATE)
B. ESS AC / ESS DC BUSES................................................................AUTO
C. CABIN PRESSURE CONTROL ...................................................MANUAL
OPERATING MANUAL
05-12-00 EXPANDED ABNORMAL / EMERGENCY PROCEDURES
Page 4
May 30/02
Revision 7
AT POWER DISTRIBUTION BOX (PDB):
CAUTION
DO NOT ATTEMPT TO RESET ANY POPPED
CIRCUIT BREAKERS.
D. AC ESS / DC ESS CBs ..............PULL AND RESET ONE (1) AT A TIME
Pull CBs one at a time, allow sufficient time (approximately thirty (30)
seconds) for smoke to stop, then reset CB.
CAUTION
PULLING THE DC ESS PILOT 2 CB WILL DISABLE
MANUAL CONTROL OF THE PRESSURIZATION
SYSTEM. RESELECT AUTO CONTROL MODE IF
PULLING THIS CB STOPS THE SMOKE.
IF SMOKE STOPS AFTER ANY ONE (1) CB IS PULLED:
12. Airplane ................PROCEED TO NEAREST SUITABLE AIRPORT AND LAND
NOTE:
See Section 05-07-70, Bus Fault - AC or DC RESET
Light On, to assist determining items inoperative with a
specific CB pulled.
13. Yaw Damper / Mach Trim Limitations ...............OBSERVE AS APPROPRIATE
See Section 01-27-30, Yaw Damper, and Section 01-22-10, Mach Trim
Compensation / Electric Elevator Trim.
14. CABIN PRESSURE CONTROL....................................................................AUTO
If available: AC ESS PILOT φA CB on PDB.
15. Windshield Heat (WSHLD) ...............OFF FOR TWO (2) SECONDS, THEN ON
16. FGC CBs..............................................PULL AND/OR RESET AS NECESSARY
• FGC #1: Copilot’s Overhead Panel, A-7
• FGC #2: Copilot’s Overhead Panel, B-7
IF SMOKE STILL CONTINUES:
17. Airplane Systems....................................................CONFIGURE AS FOLLOWS
A. Electrical System...................RETURN TO NORMAL CONFIGURATION
B. Windshield Heat (WSHLD).....OFF FOR TWO (2) SECONDS, THEN ON
C. FGC CBs .........................................PULL AND RESET AS NECESSARY
• FGC #1: Copilot’s Overhead Panel, A-7
• FGC #2: Copilot’s Overhead Panel, B-7
D. Another Source of Smoke...................................ATTEMPT TO LOCATE
E. Airplane .....PROCEED TO NEAREST SUITABLE AIRPORT AND LAND
OPERATING MANUAL
EXPANDED ABNORMAL / EMERGENCY PROCEDURES 05-12-00
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May 30/02
Revision 7
OPERATING MANUAL
THIS PAGE IS INTENTIONALLY LEFT BLANK.
05-12-00 EXPANDED ABNORMAL / EMERGENCY PROCEDURES
Page 6
May 30/02
FIRE DETECTION SYSTEM
05-13-10: Engine Fire Warning System Malfunction
ENG FIRE LOOP ALRT (RED)
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. The possibility also exists that a system fault
could develop which causes a signal output similar to a fire warning, i.e., the FIRE TEST
panel’s LOOP A or LOOP B light illuminated red, but not both illuminated. In cases such
as these, a fire could develop without triggering fire warnings, or false FIRE TEST panel
indications could be presented, again without a fire warning.
The pilot would be alerted to activation of a single fire loop by illumination of the
applicable LOOP light on the FIRE TEST panel, and by display of the red ENG FIRE
LOOP ALRT warning message on CAS, accompanied by the associated three chime
aural warning tone. Should these messages and annunciations occur, re-test the fire
warning system. If the system test is not satisfactory, the loop has failed and the fire
indication is genuine the ENGINE FIRE checklist should be executed. If the system test
is satisfactory, the fire indication is false and the faulty loop should be disabled.
SINGLE FIRE TEST LOOP LIGHT:
1. Illuminated FIRE TEST Switchlight..........................................................PRESS
IF WARNINGS ILLUMINATE, PERFORM STEPS 2 AND 3. IF WARNINGS DO NOT
ILLUMINATE, PERFORM STEPS 4 AND 5.
IF WARNINGS ILLUMINATE:
2. FIRE TEST Switchlight .........................................................................RELEASE
3. Faulty LOOP..DISABLE WITH FAULT SWITCH ON FIRE DETECTION PANEL
IF WARNINGS DO NOT ILLUMINATE:
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湾流4操作手册 Gulfstream IV Operating Manual 3(101)
