TM 1-1520-238-23P C06
SECTION II
3
4
5
2
1
9
8
10
7
11
6
1
2
4
12
1
2
22
21
15
19
18
37
23
4
1
2
24
4
25
20
17
4
4
24
33
35
27
32
4
31
4
36
1
2
18
38
28
26
1
2
2
1
34
13
4
14
16
16
30
29
M09-104H
Figure 651.
Group 11 Linkage Installation, Tail Rotor Mid Fuselage (FS 164 to FS 216)
7–311523000
