TM 1-1520-238-23
2-266
Change 3
2.76.
MAIN LANDING GEAR LEFT SHOCK STRUT STRUCTURAL SUPPORT
REMOVAL/INSTALLATION – continued
(8) Remove shear bolt (26), self-locking nut (27),
and washer (28) from support (5).
(9) Remove angle (29) from support (5).
(a) Remove two shear bolts (30), self-locking
nuts (31), and washers (32) from angle
(29).
(10) Remove three shear bolts (33), self-locking
nuts (34), and washers (35) from support (5).
(11) Remove support (5) from airframe (2).
2.76.4. Cleaning
a. Wipe removed and attaching parts and sur-
faces with a clean rag.
2.76.5. Inspection
a. Check mounting surface, support, and angle
for corrosion (para 1.49).
WARNING
If support is cracked, replace attach-
ing bolts.
b. Check support and angle for bends and/or
cracks (para 2.12).
c. Check mounting surface for broken or
stripped
threads
of
nutplates
(TM 1-1500-204-23).
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M04-3744-4A
33
35
34
2
5
26
30
29
32
31
27
28
