F 『
E C F M E
E E
E 56 E
E E
CHAPTER 75
__________
AIR
TABLE OF CONTENTS
_________________
SUBJECT_______ CH/SE/SU _ PAGE EFFECTIVITY
________ C ____ ___________ Actuator on Engine 2 Bleed Bias System on Engine 1 251 ALL Bleed Bias System on Engine 2 252 ALL Bleed Bias System on Engine 1 253 ALL Bleed Bias System on Engine 2 254 ALL
VARIABLE STATOR VANE SYSTEM (VSV) 75-32-00
FAULT ISOLATION PROCEDURES 201 ALL Failure of the VSV System on 201 ALL Engine 1 Failure of the VSV System on 203 ALL Engine 2 Loss of the feedback Signal from 205 ALL the VSV through the two Channels on Engine 1 Loss of the feedback Signal from 208 ALL the VSV through the two Channels on Engine 2 Loss of the feedback Signal from 211 ALL the VSV through the Channel A on Engine 1 Loss of the feedback Signal from 214 ALL the VSV through the Channel A on Engine 2 Loss of the feedback Signal from 217 ALL the VSV through the Channel B on Engine 1 Loss of the feedback Signal from 220 ALL the VSV through the Channel B on Engine 2 Failure of the VSV System on 223 ALL Engine 1 Failure of the VSV System on 225 ALL Engine 2
NACELLE TEMPERATURE INDICATING 75-41-00
FAULT ISOLATION PROCEDURES 201 ALL High Nacelle Temperature 201 ALL Indication on Engine 1 High Nacelle Temperature 206 ALL Indication on Engine 2 Nacelle Temperature above 310 211 ALL deg.C (590 deg.F) or Loss of the Nacelle Temperature Data on Engine 1 Nacelle Temperature above 310 213 ALL
75-CONTENTS Page 4 Aug 01/01 R CES
F 『
E C F M E
E E
E 56 E
E E
CHAPTER 75__________
AIR
TABLE OF CONTENTS_________________
SUBJECT_______ deg.C (590 deg.F) or Loss of the Nacelle Temperature Data on Engine 2 CH/SE/SU________ C_ PAGE EFFECTIVITY____ ___________
75-CONTENTS Page 5 Aug 01/01
CES AIR - FAULT SYMPTOMS
F 『
E C F M E
E E
E 56 E
E E
____________________
F T T 『
E E CFDS FAULT MESSAGES E FAULT E
E WARNINGS/MALFUNCTIONS 十 T T T 1 ISOLATION E
E ESOURCE E MESSAGE E ATA ECE PROCEDURE E
十 十 十 十 十 十 1 R EENGINE - ENG 1 NACELLE E E E E E754100 P 201E R ETEMP indication flashingE E E E ET 810 805 E R Egreen E E E E E E
Eassociated with E E E E E E R EENGINE - ENG 1 NACELLE E E E E E E R ETEMP indication flashingE E E E E E R Egreen E E E E E E
十 十 十 十 十 十 1 R EENGINE - ENG 2 NACELLE E E E E E754100 P 206E R ETEMP indication flashingE E E E ET 810 806 E R Egreen E E E E E E
Eassociated with E E E E E E R EENGINE - ENG 2 NACELLE E E E E E E R ETEMP indication flashingE E E E E E R Egreen E E E E E E
E 1 1 1 1 1 E
F 『 EEFF : ALL E Page 101∞∞75-OBSV ∞∞∞∞∞∞∞∞∞∞
E E May 01/00 E E ECES
E AIR - FAULT SYMPTOMS
F 『
E C F M E
E E
E 56 E
E E
____________________
F T T 『
E E CFDS FAULT MESSAGES E FAULT E
E WARNINGS/MALFUNCTIONS 十 T T T 1 ISOLATION E
E ESOURCE E MESSAGE E ATA ECE PROCEDURE E
十 十 十 十 十 十 1
E EEIU1FADEBLD SNSR, J15, ECU ENG1AE753180E3E753000 P 237E
E E E E E ET 810 831 E
十 十 十 十 十 十 1
E EEIU1FADEBLD SNSR, J15, ECU ENG1BE753180E3E753000 P 251E
E E E E E ET 810 839 E
十 十 十 十 十 十 1 R E EEIU1FADEHPTC VLV, J11, ECU E752110ESE752100 P 217E R E E E E E ET 810 809 E
十 十 十 十 十 十 1 R E EEIU1FADEHPTC VLV, J12, ECU E752110ESE752100 P 223E R E E E E E ET 810 811 E
十 十 十 十 十 十 1 R E EEIU1FADELPTC VLV, J11, ECU E752210ESE752200 P 201E R E E E E E ET 810 801 E
十 十 十 十 十 十 1 R E EEIU1FADELPTC VLV, J12, ECU E752210ESE752200 P 209E R E E E E E ET 810 803 E
十 十 十 十 十 十 1
E EEIU1FADETBV VLV, J11, ECU ENG1A E752310ESE752600 P 201E
E E E E E ET 810 801 E
十 十 十 十 十 十 1
E EEIU1FADETBV VLV, J12, ECU ENG1B E752310ESE752600 P 204E
E E E E E ET 810 802 E
十 十 十 十 十 十 1
E EEIU1FADEVBV ACT, HMU ENG1A E753110E1E753000 P 201E
E E E E E ET 810 801 E
十 十 十 十 十 十 1
E EEIU1FADEVBV ACT, HMU ENG1B E753110E1E753000 P 239E
E E E E E ET 810 837 E
十 十 十 十 十 十 1 R E EEIU1FADEVBV SNSR, J11, ECU E753170ESE753000 P 219E R E E E E E ET 810 813 E
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：A320 Trouble Shooting Manual 排故手册 大气 AIR(3)
