TM 1-1520-238-23P C02
SECTION II
32
52
61
50
33
28
51
34
35
1
19
15
21
9
20
12
11
1125
23
4
11
7
131812
11
11
22
11
14
11
10
8
16
55
56
59
60
55
56
59
60
57
58
53
54
29
31
30
40
41
36
3738
39
42
43
49
44
45
44
45
3
46
46
46
47
48
17
24
5
27
6
26
2
M09-646P
Figure 140.
Group 02 Wing Assembly, Aircraft Spar Installation
7–311130200–601 LH (Usbl Eff 83–23791 and Subs)
7–311130200–602 RH (Usbl Eff 83–23791 and Subs)
