(2)
Pan cover inboard to free outboard edge from lower flange of PSU support beam.
C. Lower Adjacent Carry-All. Compartment door for access.
(1)
Remove hinge linkage cover (Detail B).
(a)
Pull plunger of Nylatch fasteners out to unlocked position (Section B-B).
(b)
Pull cover from hinge mounting bracket.
(2)
Remove hinge linkage pin from hinge linkage (Detail A).
(a)
Press on both ends of pin at same time to release internal lock. Withdraw pin part way.
(b)
Grasp pin behind exposed shoulder and press release plug on end. Support door and withdraw pin.
(c)
Repeat steps for pin on opposite end of door and lower door to access position.
3. Remove Carry-All Compartment End Closure
A. Remove horizontal trim strip by lifting slightly and pulling bottom of strip inboard.
B. Remove vertical trim strip (Detail C) between filler panel and adjacent compartment by sliding strip upward out of tracks. Considerable hand pressure may be required.
C. Remove fasteners from splice plate located in channel of PSU support beam (Detail E).
D. Remove fastener securing upper attachment bracket to overhead support structure.
E. Support end closure assembly and withdraw slide bolt (Detail D) from filler panel. Slide bolt in located under inboard edge of adjacent compartment. Bolt may not slide freely and require driving force, use care to avoid damage.
CAUTION: RELEASE PIN IN END OF SLIDE BOLT MUST BE HELD IN RECESSED POSITION DURING REMOVAL OF BOLT.
577
Feb 15/79 BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details. 25-24-512 Page 401
Carry-All Compartment End Closure Installation 518
25-24-512 Figure 401 (Sheet 1) Feb 15/79
Page 402
BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details.
518 Carry-All Compartment End Cap Installation
Feb 15/79 Figure 401 (Sheet 2) 25-24-512
Page 403
BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details.
Carry-All Compartment End Closure Installation 518
25-24-512 Figure 401 (Sheet 3) Feb 15/79
Page 404
BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details.
F. Remove three fasteners securing end closure to tabs on PSU spacer panel.
G. Pull end closure inboard to clear pressure pad located at cabin wall. Ensure that outer seal flange of end closure clears adjacent structure, ceiling panel, bustle, or other equipment.
4. Install Carry-All Compartment End Closure
A. Insert edge of end closure under pressure pad at cabin wall and press into position. Insure that outer seal flange of end closure clears adjacent structure, ceiling panel, bustle or other equipment.
B. Support end closure and insert slide bolt (Detail D) into filler panel. Slide bolt is located under inboard edge of adjacent compartment. Bolt may require driving force, use care to avoid damage.
CAUTION: RELEASE PIN IN END OF SLIDE BOLT MUST BE HELD IN DEPRESSED POSITION DURING INSTALLATION.
C. Install fastener securing upper attachment bracket to overhead support structure.
D. Install three fasteners securing end closure to tabs on PSU spacer panel.
E. Install fasteners in splice plate in PSU support beam (Detail E).
F. Insert vertical trim strip (Detail C) into tracks between filler panel and adjacent compartment. Considerable hand pressure may be required.
G. Install horizontal trim strip by placing top of strip in recess, lift slightly and press lower edge into place.
5. Restore Airplane to Normal
A. Raise Adjacent Carry-All Compartment door to operating position (Fig. 401).
(1)
Install hinge linkage pins (Detail A).
(a)
Raise door to open position and align holes in linkage arms.
(b)
Insert pins and ensure that they are internally locked in place (Detail B).
