曝光臺 注意防騙 網(wǎng)曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費者

These fuses incorporate a time delay to regulate the spring-action closure of fuse. This prevents inadvertent setting of the fuses due to pressure surges that occur when the hydraulic system is first pressurized.

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 27-23-00
 ALL  ú ú 01 Page 10 ú Jan 20/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
757
FAULT ISOLATION/MAINT MANUAL

RUDDER AND ELEVATOR HYDRAULIC SYSTEMS
COMPONENT  SHT 102 FIG.  QTY  ACCESS/AREA  REFERENCE 
CIRCUIT BREAKER  1  FLT COMPT, OVERHEAD PANEL (P11)
AIR/GND SYS 1, C1182 1  11S15  *
AIR/GND SYS 2, C1170  1  11S19  *
FLT CONT SHUTOFF TAIL CTR, C4035 1  11H18  * 
FLT CONT SHUTOFF TAIL LEFT, C4033  1  11H17  *
FLT CONT SHUTOFF TAIL RIGHT, C4034  1  11H28  *
LANDING GEAR POS SYS 1, C1175  1  11C30  *
PCU MON MOD, C4270  1  11J11  *
PCU MON SENSOR, C4283  1  11J10  *
 L EICAS, M10181 COMPUTER - (REF 31-41-00, FIG. 101) R EICAS, M10182 POS SYS 2, C4279  1  11S23  *
FUSE - ELEVATOR CENTER HYDRAULIC SYSTEM  4  2  313AL, AFT FUSELAGE  *
FUSE - RUDDER CENTER HYDRAULIC SYSTEM  5  1  311AL, AFT FUSELAGE  * 
AIR/GND SYS 2, K203 AIR/GND SYS 1, K10388 AIR/GND SYS 1, K10107 AIR/GND SYS 1, K199 RELAY - (REF 32-09-00, FIG. 101) PANEL - (REF 24-22-00, FIG. 101) M10191 GENERATOR FIELD AND HYDRAULIC CONTROL,MODULE - PCU MONITOR, M10481  1  1  119BL, MAIN EQUIP CTR, P50  27-23-02 
SENSOR - L ELEVATOR CENTER PCA PRESSURE DIFFERENTIAL, TS5208  1 335DB  27-31-05 
DIFFERENTIAL, TS5207 SENSOR - L ELEVATOR INBOARD PCA PRESSURE 1  335DB  27-31-05 
DIFFERENTIAL, TS5206 SENSOR - L ELEVATOR OUTBOARD PCA PRESSURE  1  335DB  27-31-05 
DIFFERENTIAL, TS5204 SENSOR - LOWER RUDDER PCA PRESSURE  1  324CL  27-21-20 
DIFFERENTIAL, TS5205 SENSOR - MIDDLE RUDDER PCA PRESSURE  1  324CL  27-21-20 

* SEE THE WDM EQUIPMENT LIST
Rudder and Elevator Hydraulic Systems - Component Index
Figure 101 (Sheet 1)

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 27-23-00
 ALL  ú
 ú  17  Page 101
 ú  Dec 20/90 

BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
757 FAULT ISOLATION/MAINT MANUAL
COMPONENT SHT 102 FIG.  QTY  ACCESS/AREA  REFERENCE 
DIFFERENTIAL, TS5202 SENSOR - R ELEVATOR CENTER PCA PRESSURE  1 345DB  27-31-05 
SENSOR - R ELEVATOR INBOARD PCA PRESSURE DIFFERENTIAL, TS5201  1  345DB  27-31-05 
DIFFERENTIAL, TS5200 SENSOR - R ELEVATOR OUTBOARD PCA PRESSURE  1  345DB  27-31-05 
DIFFERENTIAL, TS5203SENSOR - UPPER RUDDER PCA PRESSURE 1  324CL  27-21-20 
SWITCH - FLT CONTROL SHUTOFF C, S5  1  1  FLT COMPT, RIGHT SIDE PANEL (P61), GEN FIELD & HYD CONT PANEL M10191  * 
SWITCH - FLT CONTROL SHUTOFF L, S4 1  1  FLT COMPT, RIGHT SIDE PANEL (P61), GEN FIELD & HYD CONT PANEL M10191  * 
SWITCH - FLT CONTROL SHUTOFF R, S6 1  1  FLT COMPT, RIGHT SIDE PANEL (P61), GEN FIELD & HYD CONT PANEL M10191  * 
VALVE - C SYSTEM RUDDER/ELEVATOR HYDRAULIC SHUTOFF, V102  2 1  BULKHEAD LEFT MAIN GEAR WHEEL WELL, AFT  27-23-01
 SHUTOFF, V103 VALVE - L SYSTEM RUDDER/ELEVATOR HYDRAULIC 2  1  BULKHEAD LEFT MAIN GEAR WHEEL WELL, AFT 27-23-01 
SHUTOFF, V101 VALVE - R SYSTEM RUDDER/ELEVATOR HYDRAULIC 2  1  BULKHEAD RIGHT MAIN GEAR WHEEL WELL, AFT 27-23-01 

* SEE THE WDM EQUIPMENT LIST
Rudder and Elevator Hydraulic Systems - Component Index
Figure 101 (Sheet 2)

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 27-23-00
 ALL  ú
 ú  02  Page 102
　
中國航空網(wǎng) www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：757 AMM 飛機維護手冊 飛行操縱 FLIGHT CONTROLS 2(99)