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10-503140-032 Datasheet, PDF (180/437 Pages) Amphenol Corporation – The Interconnection Leader
MIL-DTL-5015 Crimp Rear Release
Insert Arrangements
Amphenol
Aerospace
Front Face of Pin Insert or Rear Face of Socket Insert Illustrated
L
K
J
H
A
B
C
M
D
E
G
F
A
L
K
B
M
C
E
J
G
H
A
J
NK
H
P
G
M
L
F
E
B
C
D
B
A
EF
KL M
ST U V
C
D
GH J
N PR
W XZ
a b cd
ef
h
g
j
km
np rs
Insert Arrangement
Service Rating
Number of Contacts
Contact Size
28-18*
M = C; G, H, J, K, L = D; A, B = A; Bal. = Inst.
12
16
28-19*
H, M = B; A, B = D; Bal. = A
4
6
12
16
28-20
A
10
4
12
16
28-21
A
37
16
C
A
F
B
E
D
A
E
B
D
C
Insert Arrangement
Service Rating
Number of Contacts
Contact Size
28-22
D
3
3
4
16
32-1
A = E; B, C, D, E = D
2
3
0
12
A
E
A
D
B
C
EF
B
H
G
J
D
C
32-2*
E
32
4 16
32-3*
D
1224
0 4 12 16
A
C
E
G
I
K
L
P
O
U
W
B
D
H
F
J
MRN
S
T
V
X
32-6
A
2 3 2 16
4 8 12 16
Insert Arrangement
Service Rating
Number of Contacts
Contact Size
P
W
c
R
X
d
h eYS
j
ZT
f
k
g
aU
b
V
J
E
K
LFA
GB
M
HC
N
D
I
O
32-7
A, B, h, j = Inst.; Bal. = A
7
28
12
16
A
B
CD
E
FG
HI
J
K
L
MN
32-9
D
2
12
4
16
N
M
P
L
X
Y
W
K
Z
V
J
U
H
G
A
B
R
C
S
D
T
E
F
32-13
D
5 18 2
4
12 16 12 16
B
D
A
C
E
F
H
G
32-15
D
2
6
0
12
A
B
100˚
C
D
G
H
D
EI
JF
K PL
MR N
O
S
T
U
W
V
C
X
A
A
E
B
D
C
B
260˚
Insert Arrangement
Service Rating
Number of Contacts
Contact Size
100° Rotation
of 32-6
32-16
A
2 3 2 16
4 8 12 16
32-17
D
4
4
260° Rotation of
32-1
32-19
A = E, Bal. = D
2
3
0
12
  * Consult Amphenol, Sidney, NY for availability.
** Inactive for new design
CONTACT LEGEND 16 12 8
4
0
Contact Amphenol Aerospace for more information at 800-678-0141•www.amphenol-aerospace.com 179