ARMY TM 9-4120-380-14
NAVY EE-000-BA-MMA-010/7053-AC
AIR FORCE TO 35E9-136-21
6.7
LEFT FRAME, PANEL (CHASSIS) - Continued
REMOVAL - Continued
c.
Remove seven bolts (13), lockwashers (12), flat washers (11) and frame support (10)
d.
Remove 16 rivets (1) securing top (2) to frame (15).
e.
Remove top (2).
NOTE
Use 3/4 X 3/4 square tubing for support material.
f.
Place 17-1/4-inch (43.82 cm) brace (6) in compressor compartment to support condenser coil assembly.
g.
Place 15-15/16-inch (40.48 cm) brace (5) in condenser compartment to support evaporator coil assembly.
h.
Place 12-1/2-inch (31.75 cm) brace (4) in evaporator fan compartment to support evaporator fan assembly.
i.
j.
Remove five rivets (8) from bottom of frame.
k.
Remove 33 rivets (9) from side of frame
I.
Pry side (14) out and away from caulking
m.
Remove side frame (14).
INSTALLATION
a.
Apply caulking to rear frame (15).
b.
Place frame side (14) In mounting position.
c
Install five rivets (8) at bottom of left frame panel.
d.
Install 33 rivets (9).
e.
f.
Position top (2) onto frame sides.
g.
Install 16 rivets (1) securing top to frame.
h.
Install frame support (10) with seven bolts (13), lockwashers (12), and flat washers (11).
i.
Install rivet (7) securing captive receptacle to frame.
j.
Remove all compartment braces (4, 5, and 6).
k.
Weld top of frame to both sides (3).
I.
Grind smooth top of frame, both sides (3).
m.
Paint top of frame, both sides (3).
6-9