TM 1-1520-238-23
Change 8
2-271
2.77.
MAIN LANDING GEAR RIGHT SHOCK STRUT STRUCTURAL SUPPORT
REMOVAL/INSTALLATION – continued
2.77.3. Removal
a. Remove right main landing gear shock strut
structural support (1) from airframe (2).
(1) Remove shear bolt (3) from support (1).
(2) Remove bolt (4), self-locking nut (5), washer
(6), and two washers (7) from support (1).
(3) Remove shear bolt (8) and two bolts (9) from
support (1).
(4) Remove shear bolt (10), self-locking nut (11),
and washer (12) from support (1).
(5) Remove nine shear bolts (13), self-locking
nuts (14), and washers (15) from support (1).
(6) Remove shear bolts (16) and (17), two self-
locking nuts (18), and washers (19) from sup-
port (1). Use torque wrench adapter.
(7) Remove two shear bolts (20), self-locking
nuts (21), and washers (22) from support (1).
(8) Remove shear bolt (23), self-locking nut (24),
and washer (25) from support (1).
(9) Remove angle (26) from support (1).
(a) Remove two shear bolts (27), self-locking
nuts (28), and washers (29) from angle
(26).
(10) Remove three shear bolts (30), self-locking
nuts (31), and washers (32) from support (1).
(11) Remove support (1) from airframe (2).
2.77.4. Cleaning
a. Wipe removed and attaching parts and sur-
faces with a clean rag.
2.77.5. Inspection
a. Check mounting surface, support, and angle
for corrosion (para 1.49).
WARNING
If support is cracked, replace attach-
ing bolts.
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M04-3745-2A
7
6
5
12
11
10
3
4
9
8
1
2
M04-3745-3A
22
21
14
15
18
19
27
20
13
13
13
17
28
29
16
23
24
25
1
2
28
29
26
30
1
32
31
M04-3745-4A
