G.
Put the Airplane Back to its Usual Condition - Method 2

 (1)  
Install the right core cowl skirt fairing (AMM 54-61-00/001).

 S 414-057
 S 414-058
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 36-12-04
 ALL  ú ú 01P Page 411 ú Feb 18/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 S 444-059
 (2)  Do the activation procedure for the thrust reverser (AMM 78-31-00/201).
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 36-12-04
 ALL  ú ú 01P Page 412 ú Oct 18/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 FAULT ISOLATION/MAINT MANUAL
INDICATION

 * SEE THE WDM EQUIPMENT LIST INSTALLED ON SOME AIRPLANES

Indication - Component Index
Figure 101 (Sheet 1)

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 36-20-00
 ALL  ú ú 01 Page 101 ú Jun 15/98
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A85292
A
747-400 FAULT ISOLATION/MAINT MANUAL
COMPONENT  SHT 102 FIG.  QTY  ACCESS/AREA  REFERENCE AMM 
SENSOR - ENG 1 BLEED AIR PRESSURE, X846  2  1  452, RIGHT UPPER HALF STRUT  36-21-02 
SENSOR - ENG 2 BLEED AIR PRESSURE, X847  2  1  462, RIGHT UPPER HALF STRUT  36-21-02 
SENSOR - ENG 3 BLEED AIR PRESSURE, X994  2  1  472, LEFT UPPER HALF STRUT  36-21-02 
SENSOR - ENG 4 BLEED AIR PRESSURE, X995  2  1  482, LEFT UPPER HALF STRUT  36-21-02 
SENSOR - ENG 1 BLEED AIRFLOW, B7020  4  1  LEADING EDGE FLAPS  36-23-01 
SENSOR - ENG 2 BLEED AIRFLOW, B7021  4  1  511FB, INBOARD LEFT WING L/E  36-23-01 
SENSOR - ENG 3 BLEED AIRFLOW, B7022  4  1  611FB, INBOARD RIGHT WING L/E  36-23-01 
SENSOR - ENG 4 BLEED AIRFLOW, B7023  4  1  LEADING EDGE FLAPS  36-23-01 
SENSOR - ENG 1 BLEED AIR TEMPERATURE, X1050  2  1  452DR, MID LOWER FWD STRUT  36-22-02 
SENSOR - ENG 2 BLEED AIR TEMPERATURE, X1050  2  1  462DR, MID LOWER FWD STRUT  36-22-02 
SENSOR - ENG 3 BLEED AIR TEMPERATURE, X1050 2  1  472DR, MID LOWER FWD STRUT  36-22-02 
SENSOR - ENG 4 BLEED AIR TEMPERATURE, X1050  2  1  482DR, MID LOWER FWD STRUT  36-22-02 
SWITCH - ENG 1 BLEED AIR OVERPRESSURE, S1590  2  1  452, RIGHT UPPER HALF STRUT  36-21-03 
SWITCH - ENG 2 BLEED AIR OVERPRESSURE, S1591  2  1  462, RIGHT UPPER HALF STRUT  36-21-03 
SWITCH - ENG 3 BLEED AIR OVERPRESSURE, S1592  2  1  472, LEFT UPPER HALF STRUT  36-21-03 
SWITCH - ENG 4 BLEED AIR OVERPRESSURE, S1593  2  1  482, LEFT UPPER HALF STRUT  36-21-03
SWITCH - ENG 1 BLEED AIR OVERTEMPERATURE,  3  1  452DR, MID LOWER FWD STRUT  36-22-01 
S1618
SWITCH - ENG 2 BLEED AIR OVERTEMPERATURE,  3  1  462DR, MID LOWER FWD STRUT  36-22-01 
S1618 
SWITCH - ENG 3 BLEED AIR OVERTEMPERATURE,  3  1  472DR, MID LOWER FWD STRUT  36-22-01 
S1618 
SWITCH - ENG 4 BLEED AIR OVERTEMPERATURE,  3  1  482DR, MID LOWER FWD STRUT 36-22-01 
S1618
SWITCH - ENG 1 NACELLE ANTI-ICE, YMES001  1  1  FLT COMPT, P5 ANTI-ICE PNL, M7321  * 
SWITCH - ENG 2 NACELLE ANTI-ICE, YMES002  1  1  ANTI-ICE PNL, M7321 FLT COMPT, P5  * 
SWITCH - ENG 3 NACELLE ANTI-ICE, YMES003  1  1  FLT COMPT, P5 ANTI-ICE PNL, M7321  * 
SWITCH - ENG 4 NACELLE ANTI-ICE, YMES004 1  1  ANTI-ICE PNL, M7321FLT COMPT, P5 * 
TRANSMITTER - L DUCT PRESSURE, X1017 2  1  191NL, AIR-CONDITIONING DOOR  36-21-01 
　
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：747-400 AMM 飛機維護手冊 氣動系統 PNEUMATIC SYSTEM(154)