曝光台 注意防骗
网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者
APU Inflight Operation - Alternate Electrical Source...................EA-27
APU Inflight Operation - ELWS (Loadmeter) /
ASC 420 Procedures ...............................................................EA-29
Quick Reference Handbook
ABNORMAL / EMERGENCY PROCEDURES REVISION 7
Page ED - 2 May 30/02
Fire Extinguishing System Diagram
R
DISCH
2 1
APU
ENCLOSURE
APU
FIRE EXT
(PILOT, I-10)
ESS
DC BUS
APU
FIRE EXT
FIRE
EXT
DISCHD
2.5 LB HALON
1301/600 PSI N2
GAUGE
LEFT
ENGINE
RIGHT
ENGINE
LEFT
BOTTLE
RIGHT
BOTTLE
FIRE EXT
SHOT #2
(PILOT, H-8)
ESS
DC BUS
DISCH
1 2
L
THERMAL
DISCHARGE
LEFT
ENGINE
FUEL,
HYDRAULIC
FLUID,
GENERATOR
AND THRUST
REVERSER
DISABLED
WHEN
PULLED
THERMAL
DISCHARGE
GAUGE
5.6 LB HALON
1301/600 PSI N2
GAUGE
5.6 LB HALON
1301/600 PSI N2
RIGHT
ENGINE
FUEL,
HYDRAULIC
FLUID,
GENERATOR
AND THRUST
REVERSER
DISABLED
WHEN
PULLED
FIRE EXT
SHOT #1
(PILOT, G-8)
ESS
DC BUS
LEFT BOTTLE
RIGHT BOTTLE
APU SHOT
LEGEND
COMMON LINE
Quick Reference Handbook
REVISION 7 ABNORMAL / EMERGENCY PROCEDURES
May 30/02 Page ED - 3
Engine Fire AFM 4-12-10
For an engine fire warning (red ENG FIRE LOOP ALRT with
warning tone, accompanied by FIRE handle red lights ON, and
lights in the associated HP fuel cock), proceed as follows:
1. Warning Tone................................................................... SILENCE
2. Power Lever .............................................................................IDLE
NOTE: Verify proper engine (Left or Right).
If the fire warning light extinguishes with the power lever at idle,
test fire warning system. If system tests satisfactory and other
engine parameters are normal, there is no need to shut down the
engine. Select engine bleed air OFF on affected engine. Open
isolation valve. Maintain FL 410 or below.
If the fire warning light remains illuminated with the power lever at
idle:
3. Corresponding HP FUEL COCK ............................................SHUT
4. Fire Handle..............................................................................PULL
5. Fire Extinguisher .......DISCH 1 (TURN TO EXTREME POSITION)
If the fire warnings extinguish, test the associated fire warning
system. If fire warning messages test satisfactorily, perform
Engine Failure / Shutdown In Flight, page EC-6.
If the fire warning messages do not test satisfactorily or if the
fire warning lights remain illuminated for 30 seconds after firing
the first fire extinguisher, proceed as follows:
6. Fire Extinguisher .......DISCH 2 (TURN TO EXTREME POSITION)
7. Engine Failure / Shutdown In Flight Checklist (Page EC-6).............
.....................................................................................COMPLETE
WARNING: ENGINE MUST NOT BE RESTARTED AFTER A
FIRE WARNING; THE FIRE HANDLE MUST NOT BE PUSHED
IN.
CAUTION: THE ABOVE PROCEDURE MUST NOT BE USED
FOR IN FLIGHT TRAINING; SHUTTING DOWN AN ENGINE BY
MEANS OF THE FIRE HANDLE MAY LEAD TO ENGINE
COMPONENT DAMAGE AND VIBRATION.
END
Quick Reference Handbook
ABNORMAL / EMERGENCY PROCEDURES REVISION 7
Page ED - 4 May 30/02
Engine Fire On Ground AFM 4-12-20
1. Airplane ..................................STOPPED / PARKING BRAKE SET
2. Power Lever .............................................................................IDLE
3. HP Fuel Cock .........................................................................SHUT
4. Fire Handle..............................................................................PULL
5. Fire Extinguisher ....... DISCH 1 (TURN TO EXTREME POSITION)
6. Other Engine HP Fuel Cock...................................................SHUT
If fire warning light(s) extinguish, test fire warning circuit. If
light(s) test satisfactorily, proceed to Step 8.
If fire warning circuit does not test properly, or if fire light remains
illuminated for thirty (30) seconds:
7. Fire Extinguisher ....... DISCH 2 (TURN TO EXTREME POSITION)
8. Electric Master L, R and AUX Power ........................................OFF
9. APU Master Switch ......................................... PRESS/LIGHT OUT
10. After Ten (10) Seconds, Battery 1 and 2 Switches ...................OFF
11. Airplane ........................................................................ EVACUATE
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：
湾流4快速检查单QRH GULFSTREAM IV QUICK REFERENCE HANDBOOK 3(34)
