170
Amphenol
MIL-DTL-5015, Matrix ®
TABLE OF CONTENTS
MIL-DTL-5015, Matrix®
Table of Contents• 170
Design Characteristics, Customer Options• 171
Insert Av ailability and Identification• 172, 173
Insert Arrangement Drawings• 174 - 182
Class Descriptions, Performance Specifications• 183
Insert Alternate Positioning• 184
How to Order, Military and Commercial• 185
Shell Styles:
Wall mounting receptacle threaded MS3450 (9440)• 186
Cable connecting plug threaded MS3451 (9441)• 187
Bo x mounting receptacle threaded MS3452 (9442)• 188
Jam n ut receptacle threaded MS3454 (9444)• 189
Straight plug threaded MS3456 (9446)• 190
Straight plug, self-loc king threaded MS3459 (9816)• 191
Quick disconnect plug push-pull coupling (9817/9818)• 192
Matrix• ® 5015 with RADSOK® contacts , for high power 193
Contact inf ormation, sealing plugs, tools• 194
Protection caps, dust caps• 195-197
Additional MIL-DTL-5015 connectors off ered by Amphenol• 198
MIL-DTL-5015, Matrix® Typical Markets:
Military Vehicles• Heavy Equipment• Military Aircraft• Power Generation•
Amphenol
Aerospace
170 ContactAmphenolAerospaceformoreinformationat800-678-0141•www.amphenol-aerospace.com
New
Featured
ContactAmphenolAerospaceformoreinformationat800-678-0141•www.amphenol-aerospace.com
Amphenol
Aerospace
171
26482 83723 III 5015 26500 Pyle Printed
Circuit Board
EMI Filter
Transient Fiber Optics Options
Others
Matrix Pyle Crimp Rear
Release Matrix
Matrix 2 High Speed
Contacts
38999
I
II
III SJT
MS3450
wall mounting receptacle
MS3451
cable connecting receptacle
MS3452
box mounting receptacle
MS3454
jam nut receptacle
MS3456
plug with threaded
coupling
MS3459
plug with self-locking
coupling nut
Amphenol broadens their MS/Standard family of
connec tors with the MIL-DTL-5015 Crimp Rear
Release Series.
This series provides an alternative to the older MIL-C-5015
solder type. It bridges the gap between an old connector
stan dard and the environmental and high performance needs
of current technologies.
DESIGN CHARACTERISTICS
Medium to heavy weight cylindrical•
MS345( ) series intermateable with existing MIL-DTL-5015 • solder or crimp versions on existing equipment
Captive coupling nut mechanism, utilizes retaining rings • in combination with “L washers to prevent inadvertent
disas sembly
Multiple interlock systems ensure permanent • insert reten tion
Positive control of dielectric separation with guaranteed • ease of contact insertion
Positive contact retention provided by a closely toleranced • damage-proof metal retention clip
Completely sealed against environmental extremes with -•
• Individualcontactseals(conicalrisersonpininterface)
• Interfacialsealsbetweencontacts
• Peripheralgasketshell-to-shellseals
• Redundantrearwiresealsandinsert-to-shellseals
CUSTOMER OPTIONS
Seven mounting styles, in shell sizes 8 to 48*•
Threaded coupling or self-locking plug (MS3459) with an • internal ratcheting mechanism to prevent unmating due to
vibration and shock, eliminating the need for safety wiring
Proprietary quick disconnect plug, with or without • lanyard available
Classes include aluminum or stainless steel shells, •
or firewall capability
MS and Proprietary versions available•
Some styles are supplied to McDonnell Douglas •
Specifica tion BAN 7025, DC60 Series
Accommodation of contact sizes 0 to 16•
Over 100 insert arrangement patterns available, • accom modating from a minimum of 1 to a maximum
of 85 circuits
Alternate positioning available•
Thermocouple pin and socket contacts are available**•
NOTE: MIL-C-5015 is superceded to MIL-DTL-5015 for all Amphenol/Matrix rear
release crimp type contacts.
* Consult Amphenol, Sidney, NY for availability of shell sizes 44 and 48.
** Consult Amphenol, Sidney, NY for information on thermocouple contacts.
Amphenol® /Matrix® MS/Standard Cir cular
MIL-DTL-5015 with Crimp Rear Release Contacts
Proprietary quick disconnect
plug with/without lanyard
Amphenol
Aerospace
172 Contact Amphenol Aerospace for more information at 800-678-0141 • www.amphenol-aerospace.com
38999
2648283723 III
5015
26500 Pyle
Printed
Circuit Board
EMI Filter
Transient
Fiber Optics
Options
Others Matrix 2
Matrix Pyle
Crimp Rear
Release Matrix I II III
High Speed
Contacts SJT
MIL-DTL-5015 Crimp Rear Release
Insert Availability and Identification
Insert
Arrangement
Service
Rating
Total
Contacts
Contact Size
0 4 8 12 16
8S-1 A 1 1
10S-2 A 1 1
10SL-3 A 3 3
10SL-4 A 2 2
12S-1 A 2 2
12S-2 A 2 2
12S-3 A 2 2
12S-4 D 1 1
12-5 D 1 1
14S-1** A 3 3
14S-2 Inst. 4 4
14-3 A 1 1
14S-5 Inst. 5 5
14S-6 Inst. 6 6
14S-7 A 3 3
14S-9** A 2 2
14S-10 Inst. 4 4
14S-11 Inst. 4 4
14S-12 A 3 3
14S-13 A 3 3
16S-1 A 7 7
16-2* E 1 1
16S-3* B 1 1
16S-4* D 2 2
16-7* A 3 1 2
16S-8 A 5 5
16-9 A 4 2 2
16-10 A 3 3
16-11 A 2 2
16-12 A 1 1
16-13 A 2 2
18-1 A/Inst. 10 10
18-4 D 4 4
18-5 D 3 2 1
18-6* D 1 1
18-7* B 1 1
18-8 A 8 1 7
18-9 Inst. 7 2 5
18-10** A 4 4
18-11 A 5 5
18-12 A 6 6
18-13 A 4 1 3
18-14* A 2 1 1
18-15 A 4 4
18-16* C 1 1
18-17 Inst. 7 2 5
18-18 Inst. 7 2 5
18-19** A 10 10
18-22** D 3 3
Insert
Arrangement
Service
Rating
Total
Contacts
Contact Size
0 4 8 12 16
18-23 A/Inst. 10 10
18-24 A/Inst. 10 10
18-27• D 3 2 1
18-28• D 3 2 1
20-2 D 1 1
20-4 D 4 4
20-7 D/A 8 8
20-8 Inst. 6 2 4
20-9* D/A 8 1 7
20-14 A 5 2 3
20-15 A 7 7
20-16 A 9 2 7
20-17 A 6 5 1
20-18 A 9 3 6
20-19 A 3 3
20-21 A 9 1 8
20-22 A 6 3 3
20-24 A 4 2 2
20-27 A 14 14
20-29 A 17 17
20-32 D/A 8 8
20-33 A 11 11
22-2 D 3 3
22-4** A 4 2 2
22-5 D 6 2 4
22-6* D 3 2 1
22-7* E 1 1
22-9* E 3 3
22-10* E 4 4
22-11* B 2 2
22-12* D 5 2 3
22-14 A 19 19
22-15* E/A 6 5 1
22-17* D/A 9 1 8
22-18* D/A 8 8
22-19 A 14 14
22-21 A 3 1 2
22-22 A 4 4
22-23 D/A 8 8
22-27* D/A 9 1 8
22-30 A 19 19
22-32 D 6 2 4
22-36* D/A 8 8
24-1** D 2 1 1
24-2 D 7 7
24-4* D 4 1 3
24-5** A 16 16
24-6* D/A 8 8
* Consult Amphenol, Sidney, NY for availability
** Inactive for new design
Socket Only
ContactAmphenolAerospaceformoreinformationat800-678-0141•www.amphenol-aerospace.com
Amphenol
Aerospace
173
26482 83723 III 5015 26500 Pyle Printed
Circuit Board
EMI Filter
Transient Fiber Optics Options
Others
Matrix Pyle Crimp Rear
Release Matrix
Matrix 2 High Speed
Contacts
38999
I
II
III SJT
MIL-DTL-5015 Crimp Rear Release
Insert Availability and Identification
Insert
Arrangement Service
Rating Total
Contacts Contact Size
0 4 8 12 16
24-7 A 16 2 14
24-10 A 7 7
24-11 A 9 3 6
24-12 A 5 2 3
24-15 A 16 16
24-16* D/A 7 1 3 3
24-20 D 11 2 9
24-21* D 10 1 9
24-22 D 4 4
24-24 A 16 16
24-27* E 7 7
24-28 Inst 24 24
24-80* Inst 23 23
28-1 D/A 9 3 6
28-2 D 14 2 12
28-3* E 3 3
28-4* E/D 9 2 7
28-5* D 5 2 1 2
28-8* E/D/A 12 2 10
28-9 D 12 6 6
28-10 D/A 7 2 2 3
28-11 A 22 4 18
28-12 A 26 26
28-13 A 26 26
28-15 A 35 35
28-16* A 20 20
28-17 B/D/A 15 15
28-18* C/D/A/Inst 12 12
28-19* B/D/A 10 4 6
28-20 A 14 10 4
28-21 A 37 37
28-22 D 6 3 3
32-1 E/D 5 2 3
32-2* E 5 3 2
32-3* D 9 1 2 2 4
32-6 A 23 2 3 2 16
32-7 Inst /A 35 7 28
32-9 D 14 2 12
32-13 D 23 5 18
32-15 D 8 2 6
32-16 A 23 2 3 2 16
32-17 D 4 4
32-19 E/D 5 2 3
32-20 A 23 2 3 2 16
Insert
Arrangement Service
Rating Total
Contacts Contact Size
0 4 8 12 16
32-22* A 54 54
32-63 D 5 5
32-73 A 46 46
36-3 D 6 3 3
36-5 A 4 4
36-6 A 6 2 4
36-7 A 47 7 40
36-8 A 47 1 46
36-9 A 31 1 2 14 14
36-10 A 48 48
36-11 A 48 48
36-12 A 48 48
36-15 D/A 35 35
36-16 A 47 7 40
36-17 A 47 7 40
36-18 A 31 1 2 14 14
36-21 A 31 1 2 14 14
36-52 A 52 52
36-66* A 56 4 52
40-1 D 30 6 24
40-2* D 23 23
40-3* D 23 1 4 18
40-4* D 23 2 3 2 16
40-5* A 15 3 2 4 6
40-6* D 26 1 1 24
40-7* A/D 22 2 2 18
40-9 A 47 1 22 24
40-10* A 29 4 9 16
40-11* D 25 1 1 1 4 18
40-56 A 85 85
40-62* A 60 60
* Consult Amphenol, Sidney, NY for availability
** Inactive for new design
Amphenol
Aerospace
174 ContactAmphenolAerospaceformoreinformationat800-678-0141•www.amphenol-aerospace.com
38999
2648283723 III
5015
26500 Pyle
Printed
Circuit Board
EMI Filter
Transient
Fiber Optics
Options
Others Matrix 2
Matrix Pyle
Crimp Rear
Release Matrix I II III
High Speed
Contacts SJT
BA
BA
A
BC
D
A
B
C
D
E
FA
B
C
D
E
AB
100˚
A
B
C
A
B
CD
E
F
G
AB
AB
C
A
B
C
DE
100° Rotation
of 12S-3 250° Rotation
of 12S-3
100° Rotation
of 14S-2 250° Rotation
of 14S-2 100° Rotation
of 14S-1 260° Rotation
of 14S-1
C
BA
BA
100˚
BA
250˚
A
B
C
250˚
A
BC
D
260˚
A
B
C
A
B
C
Insert Arrangement 8S-1 10S-2 10SL-3 10SL-4 12S-1 12S-2 12S-3
Service Rating A A A*** A A A A
Number of Contacts 1 1 3 2 2 2 2
Contact Size 16 16 16 16 16 16 16
Insert Arrangement 12S-4 12-5 14S-1** 14S-2 14-3 14S-5 14S-6
Service Rating D D A Inst. A Inst. Inst.
Number of Contacts 1 1 3 4 1 5 6
Contact Size 16 12 16 16 8 16 16
Insert Arrangement 14S-7 14S-9** 14S-10 14S-11 14S-12 14S-13
Service Rating A A Inst. Inst. A A
Number of Contacts 3 2 4 4 3 3
Contact Size 16 16 16 16 16 16
Insert Arrangement 16S-1 16-2* 16S-3* 16S-4* 16-7* 16S-8
Service Rating A E B D A A
Number of Contacts 7 1 1 2 1 2 5
Contact Size 16 12 16 16 8 16 16
Front Face of Pin Insert or Rear Face of Socket Insert Illustrated
CONTACT LEGEND 16 12 8 4 0
* Consult Amphenol, Sidney, NY for availability
** Inactive for new design
*** Service rating Inst Class K
one Iron contact and one Constantan contact
A
B
C
D
B
CA
A
B
AB
A
B
C
D
E
F
GH
I
J
Insert Arrangement 16-9 16-10 16-11 16-12 16-13 18-1
Service Rating A A A A A B, C, F, G = A; Bal. = Inst.
Number of Contacts 2 2 3 2 1 2† 10
Contact Size 12 16 12 12 4 12 16
MIL-DTL-5015 Crimp Rear Release
Insert Arrangements
Contact Amphenol Aerospace for more information at 800-678-0141 • www.amphenol-aerospace.com
Amphenol
Aerospace
175
26482 83723 III 5015 26500 Pyle Printed
Circuit Board
EMI Filter
Transient Fiber Optics Options
Others
Matrix Pyle Crimp Rear
Release Matrix
Matrix 2 High Speed
Contacts
38999
I
II
III SJT
A
BC
D
A
BC
A
B
C
D
E
F
G
H
A
B
C
D
E
F
G
A
BC
D
A
BC
D
E
A
B
C
D
E
F
A
B
C
D
A
B
A
B
C
D
100˚
A
B
C
D
E
F
G
A
BC
DEF
G
H
K
J
AB
C
* Consult Amphenol, Sidney, NY for availability.
** Inactive for new design\
Socket only
one Iron contact and one Constantan contact
†† A, C = Iron; B, D = Constantan
100° Rotation
of 18-9
250° Rotation
of 18-9
100° Rotation
of 18-1
A
B
C
D
E
F
G
H
I
J
100˚
250˚
A
B
C
D
E
F
G
Insert Arrangement 18-4 18-5 18-6* 18-7* 18-8* 18-9
Service Rating D D D B A Inst.
Number of Contacts 4 2 1 1 1 1 7 2 5
Contact Size 16 12 16 4 8 12 16 12 16
Insert Arrangement 18-10** 18-11 18-12 18-13 18-14* 18-15
Service Rating A A A A A A
Number of Contacts 4 5 6 1 3 1 1 4††
Contact Size 12 12 16 8 12 4 16 12
Insert Arrangement 18-16* 18-17 18-18 18-19** 18-22** 18-23
Service Rating C Inst. Inst. A D B, C, F, G = A; Bal. = Inst.
Number of Contacts 1 2 5 2 5 10 3 10
Contact Size 12 12 16 12 16 16 16 16
CONTACT LEGEND 16 12 8 4 0
Front Face of Pin Insert or Rear Face of Socket Insert Illustrated
250˚
A
B
C
D
E
F
G
H
I
J
A
B
D
C
A
B
C
DE
F
G
H
250° Rotation
of 18-1
100° Rotation
of 18-5
250° Rotation
of 18-5
A
BC
100˚
A
BC
250˚
Insert Arrangement 18-24 18-27 18-28 20-2 20-4 20-7
Service Rating B, C, F, G = A; Bal. = Inst. D D D D A, B, G, H = D; C, D, E, F = A
Number of Contacts 10 2 1 2 1 1 4 8
Contact Size 16 12 16 12 16 0 12 16
MIL-DTL-5015 Crimp Rear Release
Insert Arrangements
Amphenol
Aerospace
176 ContactAmphenolAerospaceformoreinformationat800-678-0141•www.amphenol-aerospace.com
38999
2648283723 III
5015
26500 Pyle
Printed
Circuit Board
EMI Filter
Transient
Fiber Optics
Options
Others Matrix 2
Matrix Pyle
Crimp Rear
Release Matrix I II III
High Speed
Contacts SJT
A
B
C
D
EF
A
B
C
DE
F
GH
A
B
C
D
E
A
B
CD
EG
F
A
B
C
D
EFG
H
I
A
BC
D
E
F
AB
C
D
E
FGH
I
A
BC
AB
C
D
E
F
G
HI
A
B
C
D
E
F
A
B
C
D
AB
C
D
EF
G
H
IJ
K
L
M
N
* Consult Amphenol, Sidney, NY for availability
Insert Arrangement 20-8* 20-9* 20-14 20-15 20-16 20-17
Service Rating Inst. H = D; Bal. = A A A A A
Number of Contacts 2 4 1 7 2 3 7 2 7 5 1
Contact Size 8 16 12 16 8 12 12 12 16 12 16
Insert Arrangement 20-18 20-19 20-21 20-22 20-24 20-27
Service Rating A A A A A A
Number of Contacts 3 6 3 1 8 3 3 2 2 14
Contact Size 12 16 8 12 16 8 16 8 16 16
Front Face of Pin Insert or Rear Face of Socket Insert Illustrated
CONTACT LEGEND 16 12 8 4 0
ABC
D
E
F
G
H
J
K
L
MN
PT
SR
AB
C
D
E
F
K
H
JM
L
A
BC
A
B
C
D
A
B
CD
E
F
260° Rotation of 20-7
A
B
C
DE
F
GH
260˚
Insert Arrangement 20-29 20-32 20-33 22-2 22-4** 22-5
Service Rating A A, B, G, H = D; Bal. = A A D A D
Number of Contacts 17 8 11 3 2 2 2 4
Contact Size 16 16 16 8 8 12 12 16
A
B
C
A
BC
A
BC
D
AB
A
B
CD
E
Insert Arrangement 22-6** 22-7* 22-9* 22-10* 22-11* 22-12*
Service Rating D E E E B D
Number of Contacts 2 1 1 3 4 2 2 3
Contact Size 8 16 0 12 16 16 8 16
MIL-DTL-5015 Crimp Rear Release
Insert Arrangements
ContactAmphenolAerospaceformoreinformationat800-678-0141•www.amphenol-aerospace.com
Amphenol
Aerospace
177
26482 83723 III 5015 26500 Pyle Printed
Circuit Board
EMI Filter
Transient Fiber Optics Options
Others
Matrix Pyle Crimp Rear
Release Matrix
Matrix 2 High Speed
Contacts
38999
I
II
III SJT
ABC
D
E
F
G
H
J
K
LM
NU
V
R
S
TP
A
B
E
F
C
D
AB
C
D
E
F
GH
J
A
B
C
D
E
F
G
H
AB
C
D
E
F
G
H
J
KLM
N
P
A
B
C
* Consult Amphenol, Sidney, NY for availability
** Inactive for new design
Insert Arrangement 22-14 22-15* 22-17* 22-18* 22-19 22-21
Service Rating A D = 3; Bal. = A A = D; Bal. = A C, D, E = A: Bal. = D A A
Number of Contacts 19 5 1 1 8 8 14 1 2
Contact Size 16 12 16 12 16 16 16 0 16
CONTACT LEGEND 16 12 8 4 0
Front Face of Pin Insert or Rear Face of Socket Insert Illustrated
A
BC
D
A
B
C
D
E
FG
H
AB
C
D
E
F
G
H
J
AB
C
D
E
FG
H
A
B
C
D
E
F
G
AB
C
DE
FGH
JK
LMN
PSR
AB
C
D
E
FG
H
ABC
D
E
F
G
H
J
KLMN
P
IO
A
B
CD
E
FG
ABC
DEF
G
H
I
A
B
C
D
E
260° Rotation
of 22-5
AB
C
D
E
F
G
H
J
K
LM
N
U
V
R
S
TP
260˚
A
B
CD
E
F
260˚
A
B
B
C
D
A
Insert Arrangement 22-22 22-23 22-27* 22-30 22-32 22-36*
Service Rating A H = D; Bal. = A J = D; Bal. = A A D H = D; Bal. = A
Number of Contacts 4 8 1 8 19 2 4 8
Contact Size 8 12 8 16 16 12 16 12
260° Rotation
of 22-14
Insert Arrangement 24-1** 24-2 24-4* 24-5** 24-6* 24-7
Service Rating D D D A A, G, H = D; Bal. = A A
Number of Contacts 1 1 7 1 3 16 8 2 14
Contact Size 0 12 12 0 16 16 12 12 16
Insert Arrangement 24-10 24-11 24-12 24-15 24-16* 24-20
Service Rating A A A A A, B, F, G = D; C, D, E = A D
Number of Contacts 7 3 6 2 3 16 1 3 3 2 9
Contact Size 8 8 12 4 12 16 8 12 16 12 16
A
B
C
D
E
FG
AB
C
D
EF
G
H
J
KL
100° Rotation
of 24-5
AB
C
DE
FGH
JK
LMN
PSR
100˚
MIL-DTL-5015 Crimp Rear Release
Insert Arrangements
Amphenol
Aerospace
178 ContactAmphenolAerospaceformoreinformationat800-678-0141•www.amphenol-aerospace.com
38999
2648283723 III
5015
26500 Pyle
Printed
Circuit Board
EMI Filter
Transient
Fiber Optics
Options
Others Matrix 2
Matrix Pyle
Crimp Rear
Release Matrix I II III
High Speed
Contacts SJT
AB
C
D
E
F
G
H
JK
A
BC
D
AB
C
D
E
F
G
ABCD
EFGHJ
KL
M
NP
Q
RST
U
V
WXYZ
AB
C
D
E
F
G
H
J
A
B
C
D
EF
G
H
J
K
L
M
N
P
A
BC
AB
CD
P
S
EFG
A
B
CD
E
A
B
C
D
E
F
G
H
J
K
L
M
250° Rotation
of 24-5
* Consult Amphenol, Sidney, NY for availability
AB
C
DE
FGH
JK
LMN
PSR
250˚
ABCD
EFGH
KLMNPQ
RSTUV
WX Z
J
Insert Arrangement 24-21* 24-22 24-24 24-27* 24-28
Service Rating D D A E Inst.
Number of Contacts 1 9 4 16 7 24
Contact Size 8 16 8 16 16 16
Insert Arrangement 24-80* 28-1 28-2 28-3* 28-4*
Service Rating Inst. A, J, E = D; Bal. = A D E G, P, S = E; Bal. = D
Number of Contacts 23 3 6 2 12 3 2 7
Contact Size 16 8 12 12 16 8 12 16
Insert Arrangement 28-5* 28-8* 28-9 28-10 28-11
Service Rating D L, M = E; B = D; Bal. = A D G = D, Bal. = A A
Number of Contacts 2 1 2 2 10 6 6 2 2 3 4 18
Contact Size 4 12 16 12 16 12 16 4 8 12 12 16
CONTACT LEGEND 16 12 8 4 0
Front Face of Pin Insert or Rear Face of Socket Insert Illustrated
A
B
C
DE
F
G
HJ
K
LM
A
B
CD
E
F
G
A
B
C
D
E
F
G
H
J
K
L
MI
N
P
R
S
T
U
V
W
X
A
B
C
D
E
F
G
H
J
K
L
M
PR
N
ST
U
V
W
X
Y
Z
ab
d
100˚
A
B
C
D
E
F
G
H
J
K
L
M
PR
N
ST
U
V
W
X
Y
Z
ab
d
AB
CDEFG
HJKLM
PRS T
N
W
XYZ
UV
abc
de
f
gh
jk
m
l
ABC
D
E
F
G
H
J
K
LM
P
Q
R
S
T
U
VN
A
BCD
EF
G
HJK
L
M
N
P
R
100° Rotation
of 28-12
Insert Arrangement 28-12 28-13 28-15 28-16** 28-17
Service Rating A A A A R = B; M, N, P = D; Bal. = A
Number of Contacts 26 26 35 20 15
Contact Size 16 16 16 16 16
MIL-DTL-5015 Crimp Rear Release
Insert Arrangements
ContactAmphenolAerospaceformoreinformationat800-678-0141•www.amphenol-aerospace.com
Amphenol
Aerospace
179
26482 83723 III 5015 26500 Pyle Printed
Circuit Board
EMI Filter
Transient Fiber Optics Options
Others
Matrix Pyle Crimp Rear
Release Matrix
Matrix 2 High Speed
Contacts
38999
I
II
III SJT
AB
C
D
E
F
G
H
J
K
L
M
AB
C
E
G
H
J
K
L
M
A
B
C
D
E
F
G
H
J
K
L
M
NP
ABCD
EFGHJ
KLMNPR
STUVWXZ
abcdef
ghjkm
nprs
* Consult Amphenol, Sidney, NY for availability
** Inactive for new design
Insert Arrangement 28-18* 28-19* 28-20 28-21
Service Rating M = C; G, H, J, K, L = D; A, B = A; Bal. = Inst. H, M = B; A, B = D; Bal. = A A A
Number of Contacts 12 4 6 10 4 37
Contact Size 16 12 16 12 16 16
CONTACT LEGEND 16 12 8 4 0
Front Face of Pin Insert or Rear Face of Socket Insert Illustrated
A
B
C
DE
F
A
B
CD
E
A
B
C
D
E
ABC
DEF
G
H
J
AB
CD
EF
GH
J
KLMN
O
PR
S
T
UV
W
I
X
A
B
C
D
E
F
G
H
I
J
K
L
M
N
O
P
R
S
T
U
V
W
X
Y
Z
a
b
c
d
e
f
g
h
j
k
AB
CDEFG
HIJK
LMN
AB
C
D
E
F
G
H
J
K
L
MN
PR
S
T
U
V
W
XY
Z
A
BC
DE
F
G
H
100˚
AB
CD
EF
GH
IJ
KLM
N
O
PR
S
T
UV
WX
A
BC
D
100° Rotation
of 32-6 260° Rotation of
32-1
CD
E
260˚
B
A
Insert Arrangement 28-22 32-1 32-2* 32-3* 32-6
Service Rating D A = E; B, C, D, E = D E D A
Number of Contacts 3 3 2 3 3 2 1 2 2 4 2 3 2 16
Contact Size 4 16 0 12 4 16 0 4 12 16 4 8 12 16
Insert Arrangement 32-7 32-9 32-13 32-15
Service Rating A, B, h, j = Inst.; Bal. = A D D D
Number of Contacts 7 28 2 12 5 18 2 4 2 6
Contact Size 12 16 4 16 12 16 12 16 0 12
Insert Arrangement 32-16 32-17 32-19
Service Rating A D A = E, Bal. = D
Number of Contacts 2 3 2 16 4 2 3
Contact Size 4 8 12 16 4 0 12
MIL-DTL-5015 Crimp Rear Release
Insert Arrangements
Amphenol
Aerospace
180 ContactAmphenolAerospaceformoreinformationat800-678-0141•www.amphenol-aerospace.com
38999
2648283723 III
5015
26500 Pyle
Printed
Circuit Board
EMI Filter
Transient
Fiber Optics
Options
Others Matrix 2
Matrix Pyle
Crimp Rear
Release Matrix I II III
High Speed
Contacts SJT
AB
CDE
FGHJ
KLM
NO
PR
STUVW
XYZa
bcdef
ghjk
mnpr
tq
suv
xy
zAA
AB AC
AD AE
AF AG
w
123
4
5
6
7
8
9
1011
12
13
14
15
16
17
18 19 20 21
22 23
24
25
26
27
28
29
30
31
32
33
34
35 36
37
38
39
40
41
42
43
44 45
46
A
B
C
D
E
F
A
B
C
D
A
B
C
D
E
F
AB
CDE
FG
HIJ
KLMN
OPRST
UVW X
YZab
c
defg
hjkm
np
r
t
s
uv
xy
z
w
A
BC
DE
F
GH
IJKL
M
NOPR
STUV
WXYZa
bcde
fg hj
k
mnpr
t
u
vw
s
xy
z
A
B
C
D
E
F
G
H
I
J
K
L
M
N
O
P
R
S
T
U
V
W
X
Y
Z
a
b
c
d
e
f
AB
CDEFG
HJKLMN
OPQR STU
VWXYZab
c
defg hjk
mn
pr
tuvw
s
x
yz
q
100˚
AB
CD EFG
HJKLMN
OPQRSTU
VWXY Zabc
def g hj
k
mnpr
tuvw
s
x
yz
q
260° Rotation
of 32-6
* Consult Amphenol, Sidney, NY for availability
100° Rotation
of 36-10
AB
CD
EF
GH
J
KLMN
O
PR
S
T
UV
W
I
X
260˚
A
B
C
D
E
Insert Arrangement 32-20 32-22* 32-63 32-73
Service Rating A A D A
Number of Contacts 2 3 2 16 54 5 46
Contact Size 4 8 12 16 16 4 16
Insert Arrangement 36-3 36-5 36-6 36-7
Service Rating D A A A
Number of Contacts 3 3 4 2 4 7 40
Contact Size 0 12 0 0 4 12 16
Insert Arrangement 36-8 36-9 36-10 36-11
Service Rating A A A A
Number of Contacts 1 46 1 2 14 14 48 48
Contact Size 12 16 4 8 12 16 16 16
CONTACT LEGEND 16 12 8 4 0
Front Face of Pin Insert or Rear Face of Socket Insert Illustrated
MIL-DTL-5015 Crimp Rear Release
Insert Arrangements