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Feb 20/87 BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details. 25-61-311 Page 201
G. On slides without spring clamp girt bar attachment, remove latch assembly (if required).
(1)
Remove screw that attaches cable to latch assembly.
(2)
Remove self-locking straps and remove cable.
H. On aft slides with cover restraining straps, partially open cover and remove screws that attach straps to backing pan.
I. Open compartment cover.
WARNING: TO PREVENT ACCIDENTAL INFLATION OF SLIDE AND POSSIBLE INJURY TO PERSONNEL, EXTREME CARE MUST BE EXERCISED WHENEVER SLIDE IS NOT INSTALLED IN SLIDE COMPARTMENT.
J. Remove safety pin from valise pocket and insert into valve regulator housing (Detail A).
WARNING: TO PREVENT ACCIDENTAL INFLATION OF ESCAPE SLIDE AND POSSIBLE INJURY TO PERSONNEL, SAFETY PIN MUST BE INSTALLED.
K. Lift escape slide package free of velcro tape that holds it to compartment backing pan.
5. Install Escape Slide Package (Fig. 201)
CAUTION: ESCAPE SLIDE PACKAGE SHOULD BE HANDLED ONLY ON A CLEAN SURFACE. CARE SHOULD BE TAKEN NOT TO PUNCTURE OR ACCIDENTALLY INFLATE SLIDE.
A. Open compartment cover and lay compartment on floor or other horizontal surface.
B. Check that air bottle pressure gage reading is within allowable limits (Ref par. 7).
C. Lay escape slide package in compartment backing pan with girt opening centered around backing pan latch bracket.
D. Remove safety pin (Detail A) and stow in valise in pocket under flap.
CAUTION: PIN MUST BE REMOVED WHEN ESCAPE SLIDE IS INSTALLED, SO SLIDE WILL BE OPERATIVE IN EMERGENCY.
E. Inspect and lubricate latch assembly.
(1)
Make sure there is no corrosion on the latch.
(2)
Make sure there is no corrosion on the pins in the latch.
(3)
Make sure the latch operates correctly.
(4)
Spray the latch and pin with Penetrating oil (A-A-50493).
25-61-311 May 01/99 Page 202
BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details.
F. On slides with spring clamp girt bar attachment, install latch assembly (if not previously installed).
(1)
Position slide package with girt extended (Ref Fig. 201, Stage I).
(2)
If spring clamp is attached to latch cable, remove clamp from cable.
(3)
Install spring clamp over girt bar.
(4)
Check that cable length is as specified (Detail C).
(5)
On PICO slides with loop tab on lower surface of girt, thread latch cable thru loop tab on lower surface of girt.
(6)
Slip latch cable and spacer (not on all airplanes) between ends of spring clamp and install screw and nut so that screw head is towards handle side of girt.
G. On slides without spring clamp girt bar attachment, install latch assembly (if not previously installed).
(1)
Position slide package with girt extended (Ref Fig. 201, Stage I).
(2)
Check that cable length is as specified (Detail C).
(3)
Route release cable around girt bar at center of girt window and under lower surface of girt.
(4)
On PICO slides with loop tab on lower surface of girt, thread latch cable through loop tab.
(5)
Position one cable end loop on each side of hole in latch assembly with a washer on outside of each loop. Attach cable to latch assembly with screw and nut.
(6)
Tie cable segments together at a point approximately 0.5 inch from center of latch assembly screw and at a point approximately 1.5 inches from center of girt bar using self-locking straps.
H. On aft slides with cover restraining straps, attach each strap to backing pan with screw head on inner surface of pan and strap, washer, and nut on outer surface of pan.
I. Close compartment cover.
J. Lay girt on compartment cover so latch can be seen (Ref Fig. 201, Stage II).
K. Align compartment latch bracket with cover latch bracket and snap latch assembly into both latch brackets (Detail B, Fig. 201).
L. Put grit bar in retainers.
M. Check that air bottle pressure gage can be seen through inspection window.
N. Install escape slide assembly on door (Ref par. 3).
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