TM 1-1520-238-23P C06
SECTION II
3
15
23
18
17
24
15
25
20
19
3
2
4
1
2
1
11
3
7
9
10
1
21
35
34
36
33
14
15
3
4
3
5
12
2
1
2
1
4
1
2
30
29
31
32
28
27
26
8
4
16
13
22
2
6
6
37
M09-756E
Figure 652.
Group 11 Linkage Installation, Tail Rotor AFT Fuselage (FS 275 to FS 477)
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