B.
References
(1)
AIPC 28-16-04, Fig. 1
(2)
AMM 27-51-00/201, Trailing Edge Flap System
(3)
AMM 24-22-00/201, Manual Control
(4)
SSM 28-16-01
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
28-16-04
ALL ú ú 01 Page 402 ú Jun 18/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL
MAIN TANK TRANSFER VALVE ACTUATOR
SEE A
INBD
ACTUATOR MOUNTING
HOLE (4 LOCATIONS)
WASHER
(4 LOCATIONS)ADAPTER PLATE
SCREW (4 LOCATIONS)
MANUAL OVERRIDE LEVER
INDEX PLATE
BONDING JUMPER
INDEX PLATE ACTUATORMOUNTING SCREW V50, V55(3 LOCATIONS) ELECTRICAL CONNECTOR DV50, DV55
A
Main Tank Transfer Valve Actuator Installation
Figure 401
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
28-16-04
ALL ú ú 01 Page 403 ú Feb 10/94
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL
(5)
SWPM 20-20-00, Electrical Bond and Ground
(6)
WDM 28-16-11
(7)
WDM 28-16-14
C.
Access
(1)
Location Zones
573 Rear Spar to Inbd Aileron Leading Edge, Left
673 Rear Spar to Inbd Aileron Leading Edge, Right
(2)
Access Panel
573AB Inbd Aileron Actuator Access Panel
673AB Inbd Aileron Actuator Access Panel
D.
Install the Transfer Valve Actuator for the Main Tank
S 114-035
(1)
Prepare these surfaces for an electrical surface bond
(SWPM 20-20-00):
(a)
Faying surface of the index plate and valve actuator.
(b)
Faying surface of the bonding jumper and bonding jumper tab.
S 864-010
(2)
Make sure the manual override lever on the actuator is in the closed position.
S 424-011
(3)
Hold the actuator into its correct position.
S 434-026
(4)
Engage the shaft that has splines with the adapter plate.
S 434-012
(5)
Install the socket-head cap screws and the washers (4 locations) that attach the actuator to the index plate.
S 434-023
(6)
Tighten and attach a lockwire to the cap screws.
S 284-013
CAUTION: MAKE SURE THERE IS SUFFICIENT CLEARANCE BETWEEN THE MANUAL
_______ OVERRIDE LEVER AND THE ADAPTER PLATE AND THE INDEX PLATE LOCKWIRE. IF THERE IS NOT SUFFICIENT CLEARANCE WITH THE MANUAL OVERRIDE LEVER, IT CAN CAUSE THE VALVE NOT TO OPERATE AND CAUSE DAMAGE TO THE ACTUATOR MOTOR.
(7)
Look for clearance between the manual override lever and the adapter plate.
S 434-014
(8)
Connect the bonding jumper to the lug of the actuator with the bolt, washers, and nut (SWPM 20-20-00).
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
28-16-04
ALL ú ú 03 Page 404 ú Feb 18/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL
S 764-036
(9) Measure the bonding resistance between the actuator and the spar (SWPM 20-20-00).
NOTE: The resistance must not be more than 0.008 ohm.
____
S 434-015
(10)
Connect the electrical connector DV55 to the valve actuator V55 (No. 1 main tank) or the connector DV50 to the actuator V50 (No. 4 main tank).
S 714-027
(11)
Do the Main Tank Transfer Valve Test Task.
TASK 28-16-04-714-025
4. The Main Tank Transfer Valve Test (Fig. 401)_________________________________
中國(guó)航空網(wǎng) www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：747-400 AMM 飛機(jī)維護(hù)手冊(cè) 燃油 FUEL 1(191)
