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
The start valve can be manually opened and closed through an
access port in the engine cowling. See Engine Start - Manual
Operation of Start Valve, page NG-13 or refer to GIV
Maintenance Manual, Chapter 80, for procedure.
FAILURE TO CLOSE AFTER ENGINE START:
If the start valve indicator ("SVO") is still illuminated (start valve
not closed) by ground idle HP RPM, proceed as follows:
1. Start Master Switch ......................... PRESS / CHECK LIGHT OUT
2. Both Bleed Air Switches ........................................................... OFF
3. APU Air (or External Air) .......................................................... OFF
When bleed air pressure stabilizes at minimum value (minimum 30
seconds):
4. ENGINE.....................................................................SHUT DOWN
5. Notify maintenance before further start attempt.
END
Quick Reference Handbook
ABNORMAL / EMERGENCY PROCEDURES REVISION 8
Page EC - 18 Oct 11/02
Start Valve Open (SVO) Indication - In Flight AFM 3-11-30
In the event the amber SVO indication is displayed on EICAS in
flight:
1. Check all engine parameters and EVM levels.
2. If normal, investigate after landing.
3. If abnormal, shut engine down. See Engine Failure / Shutdown In
Flight, page EC-6.
END
Hot Start AFM 3-11-40
If engine exceeds maximum start temperature (700°C):
1. HP Fuel Cock (Affected Engine) ............................................SHUT
2. Affected Engine........CONTINUE TO MOTOR FOR 30 SECONDS
Continue to motor the affected engine for a maximum of thirty
(30) seconds to reduce TGT.
After a maximum of thirty (30) seconds:
3. START MASTER ......................................................................OFF
Prior to the next attempt to start, check that the fuel boost pump is
ON, fuel pressure is normal, an air source is available and its pressure
is adequate. Check wind direction and attempt to start directly into the
wind; move the airplane if required. If a second attempt produces a
hot start, shut down the affected engine. DO NOT attempt a restart.
END
Continuous (Airstart) Ignition Limitations AFM 1-74-10
For airplanes SN 1000 through 1249 without ASC 304:
The duty cycle time for continuous (airstart) ignition without ASC 304
is five (5) minutes ON and thirty (30) minutes OFF for cooling. There
is no limitation on the ignition when used in a thirty (30) seconds ON,
thirty (30) seconds OFF cycle.
Continued on next page →
Quick Reference Handbook
REVISION 7 ABNORMAL / EMERGENCY PROCEDURES
May 30/02 Page EC - 19
Continuous (Airstart) Ignition Limitations, ctd… AFM 1-74-10
For airplanes SN 1250 and subs and SN 1000 through 1249 with
ASC 304:
There is no duty cycle time limitation for continuous (airstart) ignition
with ASC 304 installed.
END
Airstart Envelope AFM FIG 1-10
Quick Reference Handbook
ABNORMAL / EMERGENCY PROCEDURES REVISION 7
Page EC - 20 May 30/02
Notes
Quick Reference Handbook
REVISION 7 ABNORMAL / EMERGENCY PROCEDURES
May 30/02 Page ED - 1
Fire / Overheat / Smoke Index
Fire Extinguishing System Diagram............................................. ED-2
Engine Fire.................................................................................. ED-3
Engine Fire On Ground ............................................................. ED-4
APU Fire ...................................................................................... ED-4
Fire In Cabin or Cockpit Area.................................................... ED-5
Electrical Smoke / Fire: Source Unknown............................... ED-6
Engine Fire Warning System Malfunction............................... ED-8
Fire Detection System Fault......................................................... ED-8
Engine Overheat......................................................................... ED-9
Pylon Hot .................................................................................... ED-9
Aft Equipment Hot.................................................................... ED-10
Converter Overheat ................................................................. ED-10
Alternator Overheat ................................................................. ED-11
Under Floor Overheat ................................................................ ED-11
Smoke and Fumes Evacuation ............................................... ED-12
Smoke In Baggage Compartment, Aft Galley, Lavatory
or Right Hand Avionics Bay................................................. ED-13
Related Topics In QRH
Master Table Of Electrical Component Availability .....................EA-22
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(33)
