- ITEM NOT ILLUSTRATED
PAGE 10016-3
25-20-31
JAN 11/2011
THIS PAGE INTENTIONALLY LEFT BLANK
FIG. ITEM PART NUMBER AIRLINE PART NO. I N D NOMENCLATURE EFF CODE UNITS PER ASSY
3 -1 5 10 15 20 25 30 BM0901D31M1-401 BMFA007-401 MS21083N4 NAS1149G0432P NAS6204-20 BMUA008-401 BMUA009-401 1 2 2 2 2 2 2 INSTALLATION KIT, DIVIDER LH RH SEAT TRACK FITTING NUT SELF LOCKING .250-28 X .219 THK WASHER, FLAT .265 DIA X .032 THK BOLT, HEX HD .250-28 X 1.620 LG INBOARD ATTACHMENT OUTBOARD ATTACHMENT *** REF 2 2 4 2 1 1
- ITEM NOT ILLUSTRATED
PAGE 10026-3
25-20-31
JAN 11/2011
THIS PAGE INTENTIONALLY LEFT BLANK
REMOVAL
1. General
The unit is an integrally bonded structure which is fabricated from sandwich panels and
aluminum extrusions. The unit cannot be disassembled without affecting its structure
integrity. Disassembly instructions found herein are limited to removal of high-wear, easily
damaged components and disassembly instructions on how to access those items requiring
repair and/or replacement.
The unit should be disassembled only to the degree necessary to replace parts, carry out
repairs and/or overhaul the unit. Complete disassembly is neither anticipated nor
recommended.
Refer to FITS AND CLEARANCES section on page 8001 for applicable torque value.
A.Removal
NOTE: CAREFULLY INSPECT ALL RIVETED SPOT WELDED, OR BONDED ASSEMBLIES AND COMPONENTS PRIOR TO DISASSEMBLY OR REMOVAL. DO NOT REMOVE THESE ITEMS UNLESS REQUIRED, DAMAGED OR NEED REPLACEMENT. IF REPLACEMENT IS REQUIRED, REFER TO SECTION 6001 OF THIS MANUAL FOR DETAILED INSTRUCTIONS.
CAUTION: EXERCISE EXTREME CARE WHEN REMOVING SCREWS OR BOLTS ATTACHING A PART TO THE SYNTHETIC PANELING. THREADED INSERTS, WHICH ARE INSTALLED IN THE PANELING TO RECEIVE SCREWS OR BOLTS, ARE INSTALLED IN PANELING WITH POTTING COMPOUND. UNNECESSARY DAMAGE TO INSERTS WILL REQUIRE REPLACEMENT.
(1) Remove unit by following “removing instructions” from figure 13001, page 13003 thru 13006.
PAGE 12001
THIS PAGE INTENTIONALLY LEFT BLANK
INSTALLATION
1. General
The unit is an integrally bonded structure which is fabricated from sandwich panels and aluminum extrusions. During assembly, it is recommended that low cost items, such as cotter pins, screws, washers, nuts, grommets, etc., be replaced when possible to prevent future maintenance requirements due to failure of such items. It is essential when replacing components, that they be identical to the items being replaced. If component substitutions are being considered, Bolder Manufacturing must be notified.
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：COMPONENT MAINTENANCE MANUAL WITH ILLUSTRATED PARTS LIST B757-200 LH RH CLASS DIVIDER(14)
