FCE Power Supply Module Installation
Figure 201
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
27-09-00
ALL ú ú 01 Page 201 ú Jun 10/92
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL
C. These are the references for the removal and installation procedures for the other FCE modules:
(1)
Flap Control Unit (FCU) - 27-51-10/201
(2)
Stabilizer Trim/Rudder Ratio Module (SRM) - 27-41-01/401
(3)
Yaw Damper Module (YDM) - 22-21-02/401
TASK 27-09-00-002-010
2. FCE Power Supply Module Removal (Fig. 201)
_______________________________
A. References
(1)
SSM 27-09-01, SSM 27-09-02
(2)
WDM 27-09-11, WDM 27-09-21
B.
Access
(1)
Location Zone
117 Main Equipment Center, LH
118 Main Equipment Center, RH
C.
Procedure
S 862-001
(1)
Open these circuit breakers and attach DO-NOT-CLOSE tags:
(a)
P7, Overhead Circuit Breaker Panel
1) 7C10, FLT CONT ELEC 2L AC
2) 7C11, FLT CONT ELEC 2L DC
3) 7C12, FLT CONT ELEC 1L AC
4) 7C13, FLT CONT ELEC 1L DC
5) 7C14, FLT CONT ELEC 1R AC
6) 7C15, FLT CONT ELEC 1R DC
7) 7C16, FLT CONT ELEC 2R AC
8) 7C17, FLT CONT ELEC 2R DC
S 022-002
(2) Remove the power supply module from the equipment shelf.
TASK 27-09-00-402-003
3. FCE Power Supply Module Installation (Fig. 201)
____________________________________
A. References
(1)
AMM 24-22-00/201, Manual Control
(2)
SSM 27-09-01
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
27-09-00
ALL ú ú 01 Page 202 ú Feb 18/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL
(3)
SSM 27-09-02
(4)
WDM 27-09-11
(5)
WDM 27-09-21
B.
Access
(1)
Location Zone
117 Main Equipment Center, LH
118 Main Equipment Center, RH
C.
Installation Procedure
S 422-004
(1)
Install the power supply module on the equipment shelf.
S 862-005
(2)
Remove the DO-NOT-CLOSE tags and close these circuit breakers:
(a)
P7, Overhead Circuit Breaker Panel
1) 7C10, FLT CONT ELEC 2L AC
2) 7C11, FLT CONT ELEC 2L DC
3) 7C12, FLT CONT ELEC 1L AC
4) 7C13, FLT CONT ELEC 1L DC
5) 7C14, FLT CONT ELEC 1R AC
6) 7C15, FLT CONT ELEC 1R DC
7) 7C16, FLT CONT ELEC 2R AC
8) 7C17, FLT CONT ELEC 2R DC
D.
PSM Faults Check
S 862-006
(1)
Supply electrical power (AMM 24-22-00/201).
S 742-008
(2)
Do a check for existing faults of the PSM:
(a)
Push the key for EXISTING FAULTS on the CMC main menu.
(b)
If <27 FCE-PSM/SPD shows on the CDU, make sure there are no PSM FAIL or PSM INVALID messages that show on the CMCS.
NOTE: If the <27 FCE-PSM/SPD message does not show, the PSM
____
operates satisfactorily.
S 862-009
(3) Remove electrical power if it is not necessary (AMM 24-22-00/201).
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
中國航空網 m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：747-400 AMM 飛機維護手冊 飛行操縱 FLIGHT CONTROLS 1(40)
