Quantcast Section V. REBUILD OF LANDING GEAR, STOWAGE BOX, STOWAGE COMPARTMENT, AND TIRE CARRIER

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95. Air Filters
a. Removal. Refer to paragraph 58b.
b.
Disassembly,
cleaning,
Inspection,
Repair,
and
Assembly.
Refer to TM 9-1827C.
c. Installation. Refer
to
paragraph
58c.
96.
Check
Valve
a. Removal. Unscrew check valve (fig. 13) and remove from
emergency relay valve.
C l e a n i n gj I n s p e c t i o n ,
Repair,
and
Assembly.
b. D i s a s s e m b l y ,
Refer to TM 9-8601.
c. Installation. Position check valve in threaded opening of
emergency relay valve and tighten.
97. Air Lines and Fittings
Air
lines
and
air
line
fittings
are
not
ordinarily
removed
except
for
replacement.
Bent, kinked, or damaged lines and
fittings must be replaced. Lines must be kept tightly attached
and
connected.
For
general
information
refer
to
TM
9-1827A.
Repair procedures for air line couplings and hose are contained
in TM 9-8601.
98.
Slack
Adjusters
(Semitrailers
M270
and
M269)
a. Removal. Refer to paragraph 64b).
b.
Disassemly, Cleaning,
Inspection,
Repair,
Assembly,
and
Testing.
Refer to TM 9-1827A.
c. Installation.
REBUILD OF LANDING GEAR, STOWAGE BOX,
Section V.
STOWAGE COMPARTMENT, AND TIRE CARRIER
99.
Landing
Gear
Note. The
key
letters
shown
in
parentheses
are
in
except
where
otherwise
indicated.
a. Disassembly of Landing Gear Left Leg Assembly.
(1)
Following
removal
procedures
outlined
in
paragraph
68b, remove left leg assembly (G, fig. 61).
(2) Remove two fillister-head screws (A) and lockwashers
(B)
which
secure
bevel
gear
cover
(C)
and
cover
gasket (E) to portion of upper leg gear housing. Re-
move cover and gasket. Discard gasket. Remove lu-
bricating
fitting
(D)
from
cover.
Rotate
bevel
gear
shaft
(AA)
to
expose
two
straight
pins
(Z)
which
secure input bevel gear (DD) on shaft, and shaft in
TAGO 1321B
138



 


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