TM 1-1520-238-23P C06
SECTION II
21
28
41
38
31
11
10
20
24
25
22
30
27
29
23
9
8
26
13
1
37
42
36
43
40
53
46
39
47
61
49
56
55
54
48
62
66
70
59
66
74
73
72
71
67
77
78
79
80
86
82
76
88
84
83
85
81
87
68
69
58
63
60
51
52
50
32
45
57
34
35
33
75
65
64
14
15
18
19
16
17
14
15
16
17
16
17
14
15
16
17
18
19
14
15
6
7
2
3
4
5
2
3
4
5
2
3
6
7
2
3
4
5
2
3
2
3
6
7
6
7
2
3
4
5
2
3
4
5
2
3
6
7
2
3
4
5
2
3
4
5
2
3
6
7
4
5
16
17
44
12
M09-644F
Figure 138.
Group 02 Wing Assembly, Aircraft Rib Installation
7–311130200–601 LH (Usbl Eff 83–23791 and Subs)
7–311130200–602 RH (Usbl Eff 83–23791 and Subs)
