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NOTE:
Allow one (1) minute after extinguisher agent
discharge for warnings to cancel.
4. APU FIRE TEST .........................................................................................PRESS
If the APU fire detection system tests properly, it may be assumed that the APU
fire has been extinguished. In flight, an expeditious descent and landing should be
considered for assessment of any damage.
If warnings have not cancelled or system does not test after warnings have been
cancelled, it must be assumed that the APU fire has NOT been extinguished.
IN FLIGHT:
5. Emergency Descent .....................................................................AS REQUIRED
See Section 05-22-20, Emergency Descent Procedure.
6. Nearest Suitable Airport............................................PROCEED TO AND LAND
ON GROUND:
7. Airplane ...............................................................STOP / SET PARKING BRAKE
8. Engines.............................................................................................SHUT DOWN
9. Fuel Boost Pumps..................................................................................ALL OFF
10. Airplane..................................................................EVACUATE AS NECESSARY
05-12-40: Fire In Cabin Or Cockpit Area
1. Oxygen Masks and Smoke Goggles ...........................................................DON
Exercise extreme caution when using oxygen near open flame.
2. GALLEY / CABIN Master Switches...............................................................OFF
IF LEVEL FLIGHT IS NOT NECESSARY:
3. Emergency Descent Procedure ................................................................BEGIN
See Section 05-22-20, Emergency Descent Procedure.
IF LEVEL FLIGHT IS NECESSARY:
4. Cruise Speed ........................................................................................MAINTAIN
IF NO FIRE IS VISIBLE IN CABIN AND IT IS NECESSARY TO OVERCOME SMOKE
OR FUMES:
5. Passenger Oxygen Masks ................................................MANUALLY DEPLOY
The Passenger Oxygen Masks may be manually deployed by rotating the OFF/
AUTO/MAN knob on the PASSENGER OXYGEN CONTROL PANEL to MAN.
6. Passenger Oxygen Masks .............................................VERIFY DEPLOYMENT
Visually check that an oxygen mask has deployed for each passenger. Advise
passengers to don oxygen masks.
7. Source of Fire.................................................................LOCATE / EXTINGUISH
Use portable fire extinguisher to extinguish fire.
IF FIRE CANNOT BE VISIBLY CONFIRMED AS BEING EXTINGUISHED, EVEN
THOUGH SMOKE OR FUMES HAVE DISSIPATED:
OPERATING MANUAL
EXPANDED ABNORMAL / EMERGENCY PROCEDURES 05-12-00
Page 3
May 30/02
Revision 7
8. Nearest Suitable Airport..............................................................................LAND
WARNING
MOST GAS-TYPE FIRE EXTINGUISHERS EMPLOY
CARBON DIOXIDE (CO2) AS THE EXTINGUISHING
AGENT. AFTER THE FIRE IS EXTINGUISHED,
REDUCE CONCENTRATION OF FUMES BY
ALLOWING ADEQUATE VENTILATION TO ENTER
THE CABIN. SEE SECTION 05-23-10, SMOKE AND
FUMES EVACUATION.
IF NECESSARY, AFTER FIRE HAS BEEN EXTINGUISHED:
9. SMOKE AND FUMES EVACUATION Procedure.................................CONSULT
See Section 05-23-10, Smoke And Fumes Evacuation.
05-12-50: Electrical Smoke/Fire: Source Unknown
1. Oxygen Masks (100%) and Smoke Goggles .............................AS REQUIRED
2. GALLEY / CABIN Master Switches...............................................................OFF
3. Fuel Boost Pumps....................................................................................ALL ON
4. Crossflow Valve (X FLOW) .........................................................................OPEN
5. Battery Switches (BATT 1 / BATT 2)...................................................BOTH ON
6. ESS AC BUS ..........................................................E INV (MANUALLY SELECT)
7. ESS DC BUS...........................................................BATT (MANUALLY SELECT)
8. ELECTRIC MASTER LEFT PWR, RIGHT PWR and AUX PWR...................OFF
9. E-BATTS (EMERG POWER)...........................................................................OFF
IF SMOKE STOPS:
10. Airplane Systems....................................................CONFIGURE AS FOLLOWS
A. FGC #2 Circuit Breaker (CB) ............................................................PULL
The FGC #2 CB is located on the Copilot’s Overhead Panel, B-7.
B. STANDBY ELECTRICAL POWER STBY ELEC, E INVERT and TRU......
ON
C. SYMBOL GENERATOR 2 and 3 CONTROL Switches.......................ALT
“Top Compact” displays, if desired.
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湾流4操作手册 Gulfstream IV Operating Manual 3(100)
