S 424-105
(5)
Connect the electrical connector.
S 864-008
(6)
Remove the DO-NOT-CLOSE tag and close this circuit breaker on the P11 panel:
(a) 11P9, PASS SIGN CONT
S 864-061
(7) Lift the PSU up until the latches are engaged.
TASK 25-23-01-904-062
7. Termination or Transition Spacer Panel Removal/Installation (Fig. 401)___________________________________________________________
A. Equipment
(1) Latch Release Rod - Make from 0.125-inch
diameter bye 6-inch long rod
B. Access
(1) Location Zone
200 Upper Half of Fuselage
C. Procedure - Remove the Spacer Panel
S 024-073
(1) To lower the PSU on the two sides of the spacer panel, do the steps that follow:
(a)
Put the latch release rod in the latch release access holes (2 locations) to release the latches.
(b)
Release the lanyard to lower the PSU.
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
25-23-01
ALL ú ú 01 Page 411 ú May 28/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
757 MAINTENANCE MANUAL
S 024-106
(2)
Loosen the wing nuts on the inboard side while you hold the spacer panel.
S 024-063
(3)
Turn the retaining clamps to loosen the PSU support structure.
S 024-107
(4)
Lower the spacer panel down. Remove the retaining springs from the air conditioning extrusion.
S 024-066
(5)
Remove the spacer panel.
D. Procedure - Install the Spacer Panel (Fig. 401)
S 864-067
(1)
Put the outboard edge of the spacer panel on the air conditioning extrusion.
S 424-108
(2)
Install the retaining springs to the index holes in the air conditioning extrusion.
S 864-069
(3)
Apply hand pressure in the outboard direction and lift the spacer panel up.
S 424-070
(4)
Turn the retaining clamps to engage the PSU support structure.
(5)
Tighten the wing nuts on the inboard side.
(6)
Lift the PSU up until the latches are engaged.
S 424-109
S 864-071
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
25-23-01
ALL ú ú 01 Page 412 ú May 28/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
757 MAINTENANCE MANUAL
CLOSETS AND PARTITIONS - DESCRIPTION AND OPERATION
__________________________________________________
1. General_______
A. Closets
_______
(1) Closets are located aft of the No. 1 (right) and No. 2 (left and right) passenger doors.
B. Partitions
__________
(1)
A windscreen is located by the No. 2 (right) and No. 4 (left and right) passenger door to protect passengers from exposure to the wind when boarding or disembarking.
(2)
Curtains slide in overhead tracks to enclose the forward, mid, and aft galley areas in the passenger compartment.
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
25-24-00
ALL ú ú 12 Page 1 ú Jun 20/96
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
757 MAINTENANCE MANUAL
WINDSCREENS - REMOVAL/INSTALLATION
__________________________________
1. General_______
A. This procedure contains two tasks. The first task is the procedure to remove the windscreen. The second task is to install the windscreen.
TASK 25-24-01-004-005
2. Remove the Windscreen (Fig. 401)_____________________
A. References
(1)
AMM 25-25-02/401, Attendant Seat
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：757 AMM 飞机维护手册 EQUIPMENT/FURNISHINGS 1(64)
