B. Position outboard support arm and clamp plate on lip of air conditioning sidewall outlet and install screws to fasten outboard support in place.
C. Engage partition with header and upper and outboard supports. Use care to avoid damaging partitions.
D. Place attachment studs in floor track, engage with track fittings on partition and tighten nut on each attachment stud.
5C8
Feb 20/85 BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details. 25-24-341 Page 401
K92451 K93081
Class Divider Partition Installation 5B3
25-24-341 Page 402 Figure 401 (Sheet 1) BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details. May 20/82
5C8 Class Divider Partition Installation
Feb 20/85 Figure 402 (Sheet 2) BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details. 25-24-341 Page 403
AFT CENTERLINE STOWAGE CLOSET - REMOVAL/INSTALLATION
1. General
A. It is necessary to remove the centerline stowage closet by disassembly before the aft lavatory sidewall panel can be removed.
2. Prepare to Remove Stowage Closet
A. Remove aft galley (Ref 25-31-71 or -81, Removal/Installation).
3. Remove Stowage Closet (Fig. 401)
A. Remove door by removing screws from door hinge.
B. Remove foot panel by removing fasteners on inside at each end.
C. Remove all shelves and upper panel by removing fasteners from support brackets.
D. Loosen fasteners behind closet securing aft panel to lavatory partition.
E. Remove fasteners inside and outside closet wall securing wall to floor.
F. Remove fasteners securing upper forward corner of wall to ceiling structure.
G. Remove wall, and aft panel from airplane.
4. Install Stowage Closet
A. Position wall and aft panel and insert aft panel under fasteners located on lavatory partition.
B. Install fasteners securing upper forward corner of wall to ceiling structure.
C. Install fasteners inside and outside closet wall securing wall to floor.
D. Tighten fasteners securing aft wall to lavatory partition.
E. Install all shelves and upper panel by installing fasteners in support brackets.
F. Install floor panel by installing fasteners on inside at each end.
G. Install door by installing screws in hinge.
5. Restore Airplane to Normal
A. Install aft galley (Ref 25-31-71 or -81, Removal/Installation).
504
May 1/76 BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details. 25-24-381 Page 401
After Centerline Stowage Closet Installation 542
25-24-381 Figure 401 May 01/76
Page 402
BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details.
CARRY-ALL COMPARTMENT AND COMPONENTS - MAINTENANCE PRACTICES
EFFECTIVITY
Carry-All Compartment Interior
1. General
A. This procedure covers the overhead stowage compartments, referred to as Carry-All Compartments, located on each side of the passenger cabin above passenger seats. Instructions and illustrations describe a typical installation. Individual compartments vary in size and configuration of attach fittings.
2. Prepare for Removal of Carry-All Compartment (Fig. 201)
A. Remove passenger service unit (Ref 25-23-511).
B. Remove bullnose cover.
(1)
Use small tool with smooth edges (not screwdriver) to pry inboard edge of bullnose cover free from support bulb located below lower edge of compartment door (Section A-A).
(a)
Start at one end by pulling, twisting and prying with tool. After end is free, pull downward, continuing to use tool as required.
CAUTION: DO NOT MOVE FREE END DOWN MORE THAN 3 INCHES BELOW BULB TO AVOID DAMAGE TO OUTBOARD LIP OF BULLNOSE.
(b)
Complete removal of inboard edge before attempting removal of outboard edge.
(2)
Pull bullnose cover inboard to free outboard edge from lower flange of PSU support beam. Work from end to end of bullnose. If bullnose retainer clips are installed squeeze protruding spring loop of retainer and move retainer upward to allow lip of bullnose to move inboard.
CAUTION: TO AVOID DAMAGE TO OUTBOARD LIP OF BULLNOSE COVER, DO NOT PULL DOWNWARD ON INBOARD EDGE TO REMOVE.
C. Lower Carry-All Compartment door for access. (Doors With Removable Pin).
(1)
Remove hinge linkage cover (Detail B).
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