TM 1-1520-238-23P
SECTION II
6
1
19
3
7
4
5
20
33
24
22
2
16
9
8
10
15
14
18
17
12
11
13
28
45
44
35
40
37
39
43
30
33
27
31
34
28
29
26
41
42
21
25
26
32
36
38
23
24
25
VIEW LOOKING DOWN
M09-645B
Figure 139.
Group 02 Wing Assembly, Aircraft Skin and Stringer Panel Installation
7–311130200–601 LH (Usbl Eff 83–23791 and Subs)
7–311130200–602 RH (Usbl Eff 83–23791 and Subs)
