46www.conesys.com sales@aero-electric.com
MIL–DTL– 5015 S III
– –
MIL-DTL-5015
Features and Application
Series III (Rear Release)
www.conesys.com sales@aero-electric.com
Features and Application
The threaded coupling, environmentally sealed
MIL-DTL-5015 Series III connector with rear-removable
crimp contacts was developed to replace the earlier solder
type. This redesigned connector is intermateable and
intermountable with the MIL-DTL-5015 Series I solder type
(MS310*) as well as the MIL-DTL- 83723 Series II (USAF)
crimp type and MIL-DTL-5015 Series II Front Release
(MS340*). Thus, it provides for a minimum effort and high
economy upgrade for existing applications.
These connectors are recommended for a wide range of
applications, from commercial/industrial and mass
transportation systems to the most stringent high reliability
defense and aerospace requirements.
This family of connectors is offered in four receptacle
mounting configurations. They include two square flange
receptacles, both wall and box mounting; cable connecting
receptacles; and jam nut receptacles which incorporate “O”
ring seals, designed for rear panel “D” hole mounting.
Two plug styles are offered - standard plug with captivated
coupling nut retained by a combination “L” washer and
retaining ring to prevent inadvertent disassembly and a
self-locking, anti-decoupling plug, which eliminates the need
for safety wiring.
Eighty-eight insert arrangements per MIL-STD-1651 are tooled
and qualified to MIL-DTL-5015, utilizing 1 to 85 contacts.
Contacts come in sizes 16, 12, 8, 4 and 0, terminating wire
sizes from 20 gauge to 0 gauge.
These connectors are available in wide range of shell
materials and finishes. Aluminum shells are offered in
both electroless nickel and olive drab cadmium to both
commercial and MS callouts. Other finishes such as anodic
and zinc nickel are available upon request to commercial
callouts only. In addition, we offer passivated stainless steel
shells with both standard and firewall-rated inserts, and
carbon steel shells with firewall inserts.
Lockwiring Eliminated – Self-locking plug eliminates the
need for lockwiring.
Universal I/R Tool – A single, expendable plastic tool is used
for both insertion and removal of contacts.
Insert Polarization – Alternate insert clocking positions aid
in mating of adjacent connectors having identical insert
arrangement.
Closed-Entry Socket Insert – Hard dielectric socket face has
lead-in chamfers for positive alignment of pins (even partially
bent within pre-established limits) with sockets.
Interfacial Pin Insert Seal – Raised moisture barriers
around each pin, which mate into lead-in chamfers of hard
face socket insert, provide individual contact sealing.
Interfacial seal is never touched by service tools.
Elastomer Wire Sealing Grommet – Sealing over a wide
range of wire diameters is assured by a triple wire seal in each
cavity at the rear of the connector.
Superior Contact Stability – Rear release crimp contact
system features a stamped beryllium-copper retaining clip
captivated by molded-in shoulders of each contact cavity in
the insulator. A rear-inserted M81969 plastic tool expands
the tines beyond the shoulder, releasing the contact.
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MIL–DTL– 5015 S III
MIL-DTL-5015
Performance Specifications
MS345*/AE55*
– –
Performance Specifications
Operating Temperature Range
Classes KS and LS: -55°C to +200°C (-67°F to +392°F)
Classes KT and W: -55°C to +175°C (-67°F to +347°F)
Class L: -55°C to +200°C (-67°F to +392°F)
Class A*: -55°C to +200°C (-67°F to +392°F)
Material and Finish Data (Class)
KT– carbon steel shell, olive drab cadmium, firewall
KS – stainless steel shell, passivated, firewall
L–aluminum shell, electroless nickel finish
LS – stainless steel shell, passivated
W–aluminum shell, olive drab cadmium over nickel base
A* – aluminum shell, black anodized finish
Corrosion Resistance
Classes KS and LS withstand 1,000-hour salt spray.
Class KT withstands 96-hour salt spray.
Class L withstands 96-hour salt spray.
Class W withstands 1,000-hour salt spray.
Environmental Seal
Wired, mated connectors with specified accessories
attached, shall meet the altitude-immersion test specified in
MIL-DTL-5015.
Durability
Minimum of 100 mating cycles
Voltage Rating
Shock and Vibration Requirements
Wired, mated connectors shall not be damaged, coupling
ring shall not loosen, and there shall be no interruption of
electrical continuity longer than 10 microseconds when
subjected to the following:
Shock
Mated connectors withstand a pulse of approximate half
sine wave of 50 G magnitude with duration of 11 milliseconds
applied in three axes per MIL-STD-1344, method 2004,
test condition A.
Vibration
Mated connectors withstand the following vibration levels:
●Random vibration per MIL-STD-1344, method 2005,
and test condition VI, letter J.
Shell-to-Shell Conductivity
Maximum potential drop shall not exceed:
●Class W = 5 millivolts
●All other classes (except A*) = 50 millivolts
Fluid Resistance
Connectors resist specified immersions in MIL-PRF-7808
(lubricating oil), MIL-PRF-23699 (lubricating oil),
MIL-PRF-5606 (hydraulic fluid), M2-V Chevron oil,
Coolanol 25, MIL-DTL-83133 (turbine fuel JP-8),
MIL-DTL-5624 (turbine fuels JP-4 and JP-5), SAE-AMS1424
Type I (defrosting fluid), and other solvents and cleaning
agents.
* Not MS approved, available to Aero-Electric part number only.
**To be used by designer only as a guide.
Service
Rating
Maximum Operating Voltage** Test Voltage Test Voltage Test Voltage Test Voltage
(Sea Level) Sea Level 50,000 Ft 70,000 Ft. 110,000 Ft.
AC (RMS) DC V RMS V RMS V RMS V RMS
Inst. 200 250 1000 400 260 200
A 500 700 2000 600 360 200
D 900 1250 2800 675 400 200
E 1250 1750 3500 750 440 200
B 1750 2450 4500 825 480 200
C 3000 4200 7000 975 560 200
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MIL–DTL– 5015 S III
MIL-DTL-5015 Series III
Part Number Development
Rear Release
Military and Aero-Electric Part Number Development
– –
Note 1: Each connector is furnished with contacts unless
ordered less contacts (L/C) as follows: One spare contact for
inserts requiring 2 to 26 of each contact and two spares for
inserts with 27 or more of each size, and a minimum of one
sealing plug up to 15% of the number contacts. No spares
or seal plugs are provided with one contact layouts. No
spares or seal plugs for contact sizes 0 and 4 are provided.
For contact size 8, no contact spares are provided, but seal
plugs are included. In addition, one insertion/removal tool
of each size is included.
Note 2: KS and KT firewall classes are only available to
Military part numbers for shell types MS3450, MS3456 and
MS3459. KS and KT classes are available to Aero callouts for
AE551 and 554, but not for AE552 (box mount receptacle).
Note 3: Proper part number marking has no “0” in front
of single digit (numeric) shell size (8S) and no “0” in front
of single digit layout. Examples: MS3450W8S-1S and
MS3450W24-2PW. Please note that J or JAN marking has
been deleted as of August 12, 2008.
Mil. Prefix MS34 50 L 14S - 5 P X
Aero Prefix AE5 50 L 14S - 5 P X -340
Shell Type
50 = Wall mount receptacle
51 = Cable connecting receptacle
52 = Box mount receptacle
54 = Jam nut receptacle
56 = Straight plug
59 = Self-locking plug
Class (Material and Finish)
A= Aluminum shell, black anodized finish (Aero part number only)
KS = Stainless steel shell, passivated, firewall (n/a in MS3451, MS3452, MS3454)
KT = Carbon steel shell, cadmium finish, firewall (n/a in MS3451, MS3452, MS3454)
LS = Stainless steel shell, passivated
L= Aluminum shell, electroless nickel finish
W= Aluminum shell, olive drab cadmium over electroless nickel base
Shell Size
8S, 10S, 10SL, 12, 12S, 14, 14S, 16, 16S, 18, 20, 22, 24, 28, 32, 36 or 40
Insert Arrangement
See pages 58 thru 68
Contact Style
P= Pin
S= Socket
A= Pin connector less pins (with intent to use non-std contact)
B= Socket connector less sockets (with intent to use non-std contacts)
Polarization
N= Normal (not included in part number)
W, X, Y or Z= Alternate insert polarizations (see pages 58 thu 62 for position availability)
Modification (applies to Aero part numbers only)
01 = Less contacts (is not marked on the part)
340 = Connector kitted with M85049/31-XXX E-nut
341 = Connector kitted with M85049/52-1-XXX straight clamp
342 = Connector kitted with M85049/51-1-XXX right angle clamp
Consult factory for other modifications
49www.conesys.com sales@aero-electric.com
MIL–DTL– 5015 S III
MS3450 per AS34501
Wall Mount Receptacle
AE550
Threaded Coupling, Crimp Removable, Rear Release
– –
Note 1: L MAX is same as L MAX for AE551 on next page.
Note 2: Maximum grommet O.D. is same as ⭋E MAX for
AE551 on next page.
BLUE COLOR BANDS
J ACCESSORY THREAD
G
F
A MATING THREAD
DB
POLARIZING KEY
4x [ H HOLES
3 ACCESSORY TEETH
L
MAX
MIN FULL THREAD
.290(7.37) FOR 8S-24
.467(11.86) FOR 28-40
GROMMET
EXTENSION .190(4.83)
.130(3.30)
FOR 16 AND 12 CONTACTS
.340(8.64)
.130(3.30)
FOR 8,4, AND 0 CONTACTS
Page 48 Completed Part Number
Page 56 Contacts, Sealing Plugs and Tools
Pages 63–68 Insert Arrangements
Page 47 Performance Specifications
Pages 58–62 Insert Availability and Contact Information
Page 58 Polarization
Shell
Size
A B D F G ⭋H J
Mating Classes L, LS, W Classes KS, KT Accessory
Thread +.031 +.79 +.010 +.25 +.010 +.25 Thread
Class 2A ±.015 ±.38 -.000 -.00 (TP) ±.031 ±.79 -.005 -.13 -.005 -.13 Class 2A
inch mm inch mm inch mm inch mm inch mm inch mm
8S 1/2-28 UNEF .083 2.11 .562 14.27 .594 15.09 .875 22.23 .120 3.05 .150 3.81 1/2-20UNF
10S 5/8-24 UNEF .083 2.11 .562 14.27 .719 18.26 1.000 25.40 .120 3.05 .150 3.81 5/8-24UNEF
10SL 5/8-24 UNEF .083 2.11 .562 14.27 .719 18.26 1.000 25.40 .120 3.05 .150 3.81 5/8-24UNEF
12 3/4-20 UNEF .083 2.11 .750 19.05 .812 20.62 1.094 27.79 .120 3.05 .150 3.81 3/4-20UNEF
12S 3/4-20 UNEF .083 2.11 .562 14.27 .812 20.62 1.094 27.79 .120 3.05 .150 3.81 3/4-20UNEF
14 7/8-20 UNEF .083 2.11 .750 19.05 .906 23.01 1.188 30.18 .120 3.05 .150 3.81 7/8-20UNEF
14S 7/8-20 UNEF .083 2.11 .562 14.27 .906 23.01 1.188 30.18 .120 3.05 .150 3.81 7/8-20UNEF
16 1-20 UNEF .083 2.11 .750 19.05 .969 24.61 1.281 32.54 .120 3.05 .150 3.81 1-20UNEF
16S 1-20 UNEF .083 2.11 .562 14.27 .969 24.61 1.281 32.54 .120 3.05 .150 3.81 1-20UNEF
18 1 1/8-18 UNEF .125 3.18 .750 19.05 1.062 26.97 1.375 34.93 .120 3.05 .177 4.50 1-1/16-18UNEF
20 1 1/4-18 UNEF .125 3.18 .750 19.05 1.156 29.36 1.500 38.10 .120 3.05 .177 4.50 1-3/16-18UNEF
22 1 3/8-18 UNEF .125 3.18 .750 19.05 1.250 31.75 1.625 41.28 .120 3.05 .177 4.50 1-5/16-18UNEF
24 1 1/2-18 UNEF .125 3.18 .812 20.62 1.375 34.93 1.750 44.45 .147 3.73 .177 4.50 1-7/16-18UNEF
28 1 3/4-18 UNS .125 3.18 .812 20.62 1.562 39.67 2.000 50.80 .147 3.73 .177 4.50 1-3/4-18UNS
32 2-18 UNS .125 3.18 .875 22.23 1.750 44.45 2.250 57.15 .173 4.39 .209 5.31 2-18UNS
36 2 1/4-16 UN .125 3.18 .875 22.23 1.938 49.23 2.500 63.50 .173 4.39 .209 5.31 2-1/4-16UN
40 2 1/2-16 UN .125 3.18 .875 22.23 2.188 55.58 2.750 69.85 .173 4.39 .209 5.31 2-1/2-16UN
50www.conesys.com sales@aero-electric.com
MIL–DTL– 5015 S III
MS3451 per AS34511
Cable Connecting Receptacle
AE551
Threaded Coupling, Crimp Removable, Rear Release
– –
[ S[ E
MAX
GROMMET
BLUE COLOR BANDS V ACCESSORY THREAD
A
MATING THREAD
M
L
MAX
R
ACROSS FLATS
3 ACCESSORY TEETH
MIN FULL THREAD
.290(7.37) FOR 8S-24
.467(11.86) FOR 28-40
.083±.015(2.11±.38) FOR 8S-16S
.125±.015(3.18±.38) FOR 18-40
GROMMET
EXTENSION .190(4.83)
.130(3.30)
FOR 16 AND 12 CONTACTS
.340(8.64)
.130(3.30)
FOR 8,4, AND 0 CONTACTS
POLARIZING KEY
Shell
Size
A⭋E L MAX M R ⭋S V
Mating Thread 16 & 12 8, 4 & 0 +.031 +.79 Accessory Thread
Class 2A Maximum Contacts Contacts -.000 -.00 ±.031 ±.79 Class 2A
inch mm inch mm inch mm inch mm inch mm inch mm
8S 1/2-28 UNEF .305 7.75 2.031 51.59 ––.562 14.27 .504/.496 12.80/12.60 .729 18.52 1/2-20UNF
10S 5/8-24 UNEF .405 10.29 2.031 51.59 ––.562 14.27 .629/.621 15.98/15.77 .854 21.69 5/8-24UNEF
10SL 5/8-24 UNEF .405 10.29 2.031 51.59 ––.562 14.27 .629/.621 15.98/15.77 .854 21.69 5/8-24UNEF
12 3/4-20 UNEF .549 13.94 2.125 53.98 ––.750 19.05 .754/.746 19.15/18.95 .974 24.74 3/4-20UNEF
12S 3/4-20 UNEF .549 13.94 2.031 51.59 ––.562 14.27 .754/.746 19.15/18.95 .974 24.74 3/4-20UNEF
14 7/8-20 UNEF .665 16.89 2.125 53.98 ––.750 19.05 .879/.871 22.33/22.12 1.099 27.91 7/8-20UNEF
14S 7/8-20 UNEF .665 16.89 2.031 51.59 ––.562 14.27 .879/.871 22.33/22.12 1.099 27.91 7/8-20UNEF
16 1-20 UNEF .790 20.07 2.125 53.98 2.500 63.50 .750 19.05 1.005/.996 25.53/25.30 1.224 31.09 1-20UNEF
16S 1-20 UNEF .790 20.07 2.031 51.59 ––.562 14.27 1.005/.996 25.53/25.30 1.224 31.09 1-20UNEF
18 1 1/8-18 UNEF .869 22.07 2.125 53.98 2.500 63.50 .750 19.05 1.131/1.121 28.73/28.47 1.349 34.26 1-1/16 -18UNEF
20 1 1/4-18 UNEF .994 25.25 2.125 53.98 2.500 63.50 .750 19.05 1.256/1.246 31.90/31.65 1.474 37.44 1-3/16-18UNEF
22 1 3/8-18 UNEF 1.119 28.42 2.125 53.98 2.500 63.50 .750 19.05 1.381/1.371 35.08/34.82 1.599 40.61 1-5/16-18UNEF
24 1 1/2-18 UNEF 1.244 31.60 2.125 53.98 2.500 63.50 .812 20.62 1.506/1.496 38.25/38.00 1.715 43.56 1-7/16 -18UNEF
28 1 3/4-18 UNS 1.465 37.21 2.125 53.98 2.500 63.50 .812 20.62 1.756/1.746 44.60/44.35 1.974 50.14 1-3/4-18UNS
32 2-18 UNS 1.715 43.56 2.125 53.98 2.500 63.50 .875 22.23 2.007/1.996 50.98/50.70 2.224 56.49 2-18UNS
36 2 1/4-16 UN 1.930 49.02 2.125 53.98 2.500 63.50 .875 22.23 2.257/2.246 57.33/57.05 2.474 62.84 2-1/4-16UN
40 2 1/2-16 UN 2.145 54.48 2.125 53.98 2.500 63.50 .875 22.23 2.511/2.496 63.78/63.40 2.724 69.19 2-1/2-16UN
Page 48 Completed Part Number
Page 56 Contacts, Sealing Plugs and Tools
Pages 63–68 Insert Arrangements
Page 47 Performance Specifications
Pages 58–62 Insert Availability and Contact Information
Page 58 Polarization
51www.conesys.com sales@aero-electric.com
MIL–DTL– 5015 S III
MS3452
Box Mount Receptacle
AE552
Threaded Coupling, Crimp Removable, Rear Release
– –
S
R
A MATING THREAD
M
L
MAX
[ GG
4x [ T HOLES
.083±.015(2.11±.38) FOR 8S-16S
.125±.015(3.18±.38) FOR 18-40
BLUE COLOR BAND
POLARIZING KEY
Page 48 Completed Part Number
Page 56 Contacts, Sealing Plugs and Tools
Pages 63–68 Insert Arrangements
Page 47 Performance Specifications
Pages 58–62 Insert Availability and Contact Information
Page 58 Polarization
Note 1: The insulation material shall be above, flush with,
or no more than .015 inches (.38 mm) below the metal shell.
Note 2: At time of catalog printing, MS3452 was not
superseded by SAE document - AS34521.
Shell
Size
A⭋GG L MAX M R S ⭋T
Mating Thread 16 & 12 8, 4 & 0 +.031 +.79 +.010 +.25
Class 2A ±.016 ±.41 Contacts Contacts -.000 -.00 (TP) ±.031 ±.79 -.005 -.13
inch mm inch mm inch mm inch mm inch mm inch mm inch mm
8S 1/2-28 UNEF .500 12.70 1.662 42.21 ––.562 14.27 .594 15.09 .875 22.23 .120 3.05
10S 5/8-24 UNEF .625 15.88 1.662 42.21 ––.562 14.27 .719 18.26 1.000 25.40 .120 3.05
10SL 5/8-24 UNEF .625 15.88 1.662 42.21 ––.562 14.27 .719 18.26 1.000 25.40 .120 3.05
12 3/4-20 UNEF .750 19.05 1.662 42.21 ––.750 19.05 .812 20.62 1.094 27.79 .120 3.05
12S 3/4-20 UNEF .750 19.05 1.662 42.21 ––.562 14.27 .812 20.62 1.094 27.79 .120 3.05
14 7/8-20 UNEF .875 22.23 1.662 42.21 ––.750 19.05 .906 23.01 1.188 30.18 .120 3.05
14S 7/8-20 UNEF .875 22.23 1.662 42.21 ––.562 14.27 .906 23.01 1.188 30.18 .120 3.05
16 1-20 UNEF 1.000 25.40 1.662 42.21 1.937 49.20 .750 19.05 .969 24.61 1.281 32.54 .120 3.05
16S 1-20 UNEF 1.000 25.40 1.662 42.21 ––.562 14.27 .969 24.61 1.281 32.54 .120 3.05
18 1 1/8-18 UNEF 1.062 26.97 1.662 42.21 1.937 49.20 .750 19.05 1.062 26.97 1.375 34.93 .120 3.05
20 1 1/4-18 UNEF 1.187 30.15 1.662 42.21 1.937 49.20 .750 19.05 1.156 29.36 1.500 38.10 .120 3.05
22 1 3/8-18 UNEF 1.312 33.32 1.662 42.21 1.937 49.20 .750 19.05 1.250 31.75 1.625 41.28 .120 3.05
24 1 1/2-18 UNEF 1.437 36.50 1.662 42.21 1.937 49.20 .812 20.62 1.375 34.93 1.750 44.45 .147 3.73
28 1 3/4-18 UNS 1.750 44.45 1.662 42.21 1.937 49.20 .812 20.62 1.562 39.67 2.000 50.80 .147 3.73
32 2-18 UNS 2.000 50.80 1.662 42.21 1.937 49.20 .875 22.23 1.750 44.45 2.250 57.15 .173 4.39
36 2 1/4-16 UN 2.250 57.15 1.662 42.21 1.937 49.20 .875 22.23 1.938 49.23 2.500 63.50 .173 4.39
40 2 1/2-16 UN 2.500 63.50 1.662 42.21 1.937 49.20 .875 22.23 2.188 55.58 2.750 69.85 .173 4.39
52www.conesys.com sales@aero-electric.com
MIL–DTL– 5015 S III
MS3454 per AS34541
Jam Nut Receptacle
AE554
Threaded Coupling, Crimp Removable, Rear Release
– –
MIN FULL THREAD
.290(7.37) FOR 8S-24
.467(11.86) FOR 28-40
BLUE COLOR BAND
BLUE COLOR BAND
D.180(4.57)
.165(4.19)
F
MATING THREAD
H
ACCESSORY THREAD
[ .032(.81) MAX
SAFETY WIRE HOLE
(3 EQALLY SPACED)
"O" RING
A
B
[ C
SPRING PIN
MS171430
PANEL THICKNESS
.128(3.25) MAX
.196(4.98)
.186(4.72)
E
MAX
3 ACCESSORY TEETH
GROMMET
EXTENSION .190(4.83)
.130(3.30)
FOR 16 AND 12 CONTACTS
.340(8.64)
.130(3.30)
FOR 8,4, AND 0 CONTACTS
POLARIZING KEY
Page 48 Completed Part Number
Page 56 Contacts, Sealing Plugs and Tools
Pages 63–68 Insert Arrangements
Page 47 Performance Specifications
Pages 58–62 Insert Availability and Contact Information
Page 58 Polarization
Note: Maximum grommet O.D. is same as ⭋E MAX on next
page.
Shell
Size
A B ⭋C D E MAX F H
16 & 12 8, 4 & 0 Mating Thread Accessory Thread
±.005 ±.13 ±.010 ±.25 ±.005 ±.13 ±.005 ±.13 Contacts Contacts Class 2A Class 2A
inch mm inch mm inch mm inch mm inch mm inch mm
8S 1.187 30.15 .687 17.45 1.272 32.31 .720 18.29 2.031 51.59 ––1/2-28 UNEF 1/2-20UNF
10S 1.312 33.32 .812 20.62 1.397 35.48 .720 18.29 2.031 51.59 ––5/8-24 UNEF 5/8-24UNEF
10SL 1.312 33.32 .812 20.62 1.397 35.48 .720 18.29 2.031 51.59 ––5/8-24 UNEF 5/8-24UNEF
12 1.437 36.50 .937 23.80 1.522 38.66 .970 24.64 2.125 53.98 ––3/4-20 UNEF 3/4-20UNEF
12S 1.437 36.50 .937 23.80 1.522 38.66 .720 18.29 2.031 51.59 ––3/4-20 UNEF 3/4-20UNEF
14 1.562 39.67 1.125 28.58 1.647 41.83 .970 24.64 2.125 53.98 ––7/8-20 UNEF 7/8-20UNEF
14S 1.562 39.67 1.125 28.58 1.647 41.83 .720 18.29 2.031 51.59 ––7/8-20 UNEF 7/8-20UNEF
16 1.687 42.85 1.250 31.75 1.772 45.01 .970 24.64 2.125 53.98 2.500 63.50 1-20 UNEF 1-20UNEF
16S 1.687 42.85 1.250 31.75 1.772 45.01 .720 18.29 2.031 51.59 ––1-20 UNEF 1-20UNEF
18 1.812 46.02 1.375 34.93 1.897 48.18 .970 24.64 2.125 53.98 2.500 63.50 1 1/8-18 UNEF 1-1/16-18UNEF
20 1.937 49.20 1.500 38.10 2.022 51.36 .970 24.64 2.125 53.98 2.500 63.50 1 1/4-18 UNEF 1-3/16-18UNEF
22 2.156 54.76 1.625 41.28 2.241 56.92 .970 24.64 2.125 53.98 2.500 63.50 1 3/8-18 UNEF 1-5/16-18UNEF
24 2.281 57.94 1.750 44.45 2.366 60.10 .970 24.64 2.125 53.98 2.500 63.50 1 1/2-18 UNEF 1-7/16-18UNEF
28 2.531 64.29 2.000 50.80 2.616 66.45 .970 24.64 2.125 53.98 2.500 63.50 1 3/4-18 UNS 1-3/4-18UNS
32 2.781 70.64 2.375 60.33 2.866 72.80 .970 24.64 2.125 53.98 2.500 63.50 2-18 UNS 2-18UNS
36 3.031 76.99 2.625 66.68 3.116 79.15 .970 24.64 2.125 53.98 2.500 63.50 2 1/4-16 UN 2-1/4-16UN
40 3.281 83.34 2.875 73.03 3.366 85.50 .970 24.64 2.125 53.98 2.500 63.50 2 1/2-16 UN 2-1/2-16UN
53www.conesys.com sales@aero-electric.com
MIL–DTL– 5015 S III
MS3456
Straight Plug
AE556
Threaded Coupling, Crimp Removable, Rear Release
– –
Page 48 Completed Part Number
Page 56 Contacts, Sealing Plugs and Tools
Pages 63–68 Insert Arrangements
Page 47 Performance Specifications
Pages 58–62 Insert Availability and Contact Information
Page 58 Polarization
MIN FULL THREAD
.290(7.37) FOR 8S-24
.467(11.86) FOR 28-40
GROMMET
EXTENSION .190(4.83)
.130(3.30)
FOR 16 AND 12 CONTACTS
.340(8.64)
.130(3.30)
FOR 8,4, AND 0 CONTACTS
[ A
MAX
C MATING THREAD
BLUE COLOR BAND
HMAX
3x [ .035(.89)
SAFETY WIRE HOLES EQUALLY SPACED
(EXCEPT SHELL SIZES 8 TO 14 – 2 HOLES MIN)
F ACCESSORY THREAD
3 TEETH
EQUALLY SPACED
[ E
MAX
GROMMET
[ B
POLARIZING
KEYWAY
Shell
Size
⭋A⭋B C ⭋E F H MAX
Mating Thread Accessory Thread 16 & 12 8, 4 & 0
Maximum ±.005 ±.13 Class 2B Maximum Class 2A Contacts Contacts
inch mm inch mm inch mm inch mm inch mm
8S .844 21.44 .360 9.14 1/2-28 UNEF .305 7.75 1/2-20UNF 2.031 51.59 ––
10S .969 24.61 .435 11.05 5/8-24 UNEF .405 10.29 5/8-24UNEF 2.031 51.59 ––
10SL .969 24.61 .443* 11.25* 5/8-24 UNEF .405 10.29 5/8-24UNEF 2.031 51.59 ––
12 1.062 26.97 .550 13.97 3/4-20 UNEF .549 13.94 3/4-20UNEF 2.125 53.98 ––
12S 1.062 26.97 .550 13.97 3/4-20 UNEF .549 13.94 3/4-20UNEF 2.031 51.59 ––
14 1.156 29.36 .670 17.02 7/8-20 UNEF .665 16.89 7/8-20UNEF 2.125 53.98 ––
14S 1.156 29.36 .670 17.02 7/8-20 UNEF .665 16.89 7/8-20UNEF 2.031 51.59 ––
16 1.250 31.75 .800 20.32 1-20 UNEF .790 20.07 1-20UNEF 2.125 53.98 2.500 63.50
16S 1.250 31.75 .800 20.32 1-20 UNEF .790 20.07 1-20UNEF 2.031 51.59 ––
18 1.344 34.14 .925 23.50 1 1/8-18 UNEF .869 22.07 1-1/16-18UNEF 2.125 53.98 2.500 63.50
20 1.469 37.31 1.045 26.54 1 1/4-18 UNEF .994 25.25 1-3/16-18UNEF 2.125 53.98 2.500 63.50
22 1.594 40.49 1.170 29.72 1 3/8-18 UNEF 1.119 28.42 1-5/16-18UNEF 2.125 53.98 2.500 63.50
24 1.719 43.66 1.295 32.89 1 1/2-18 UNEF 1.244 31.60 1-7/16-18UNEF 2.125 53.98 2.500 63.50
28 1.969 50.01 1.515 38.48 1 3/4-18 UNS 1.465 37.21 1-3/4-18UNS 2.125 53.98 2.500 63.50
32 2.219 56.36 1.765 44.83 2-18 UNS 1.715 43.56 2-18UNS 2.125 53.98 2.500 63.50
36 2.469 62.71 1.975 50.17 2 1/4-16 UN 1.930 49.02 2-1/4-16UN 2.125 53.98 2.500 63.50
40 2.719 69.06 2.225 56.52 2 1/2-16 UN 2.145 54.48 2-1/2-16UN 2.125 53.98 2.500 63.50
* Tolerance for this dimension is ± .003(.08)
Note: At time of catalog printing, MS3456 was not
superseded by SAE document - AS34561.
54www.conesys.com sales@aero-electric.com
MIL–DTL– 5015 S III
MS3459 per AS34591
Self-Locking Plug
AE559
Threaded Coupling, Crimp Removable, Rear Release
– –
Page 48 Completed Part Number
Page 56 Contacts, Sealing Plugs and Tools
Pages 63–68 Insert Arrangements
Page 47 Performance Specifications
Pages 58–62 Insert Availability and Contact Information
Page 58 Polarization
L
MAX
[ C
MAX
B ACCESSORY THREAD
3 ACCESSORY TEETH
BLUE COLOR BAND
MIN FULL THREAD
.290(7.37) FOR 8S-24
.467(11.86) FOR 28-40
[ D[ E
MAX
GROMMET
GROMMET
EXTENSION .190(4.83)
.130(3.30)
FOR 16 AND 12 CONTACTS
.340(8.64)
.130(3.30)
FOR 8,4, AND 0 CONTACTS
A MATING THREAD
POLARIZING
KEYWAY
Shell
Size
A B ⭋C⭋D⭋E L MAX
Mating Thread Accessory Thread 16 & 12 8, 4 & 0
Class 2B Class 2A Maximum ±.005 ±.13 Maximum Contacts Contacts
inch mm inch mm inch mm inch mm inch mm
8S 1/2-28 UNEF 1/2-20UNF .963 24.46 .360 9.14 .305 7.75 2.031 51.59 ––
10S 5/8-24 UNEF 5/8-24UNEF 1.088 27.64 .435 11.05 .405 10.29 2.031 51.59 ––
10SL 5/8-24 UNEF 5/8-24UNEF 1.088 27.64 .443* 11.25* .405 10.29 2.031 51.59 ––
12 3/4-20 UNEF 3/4-20UNEF 1.213 30.81 .550 13.97 .549 13.94 2.125 53.98 ––
12S 3/4-20 UNEF 3/4-20UNEF 1.213 30.81 .550 13.97 .549 13.94 2.031 51.59 ––
14 7/8-20 UNEF 7/8-20UNEF 1.358 34.49 .670 17.02 .665 16.89 2.125 53.98 ––
14S 7/8-20 UNEF 7/8-20UNEF 1.358 34.49 .670 17.02 .665 16.89 2.031 51.59 ––
16 1-20 UNEF 1-20UNEF 1.463 37.16 .800 20.32 .790 20.07 2.125 53.98 2.500 63.50
16S 1-20 UNEF 1-20UNEF 1.463 37.16 .800 20.32 .790 20.07 2.031 51.59 ––
18 1 1/8-18 UNEF 1-1/16-18UNEF 1.588 40.34 .925 23.50 .869 22.07 2.125 53.98 2.500 63.50
20 1 1/4-18 UNEF 1-3/16-18UNEF 1.713 43.51 1.045 26.54 .994 25.25 2.125 53.98 2.500 63.50
22 1 3/8-18 UNEF 1-5/16-18UNEF 1.788 45.42 1.170 29.72 1.119 28.42 2.125 53.98 2.500 63.50
24 1 1/2-18 UNEF 1-7/16-18UNEF 1.963 49.86 1.295 32.89 1.244 31.60 2.125 53.98 2.500 63.50
28 1 3/4-18 UNS 1-3/4-18UNS 2.213 56.21 1.515 38.48 1.465 37.21 2.125 53.98 2.500 63.50
32 2-18 UNS 2-18UNS 2.463 62.56 1.765 44.83 1.715 43.56 2.125 53.98 2.500 63.50
36 2 1/4-16 UN 2-1/4-16UN 2.713 68.91 1.975 50.17 1.930 49.02 2.125 53.98 2.500 63.50
40 2 1/2-16 UN 2-1/2-16UN 2.963 75.26 2.225 56.52 2.145 54.48 2.125 53.98 2.500 63.50
* Tolerance for this dimension is ± .003(.08)
55www.conesys.com sales@aero-electric.com
MIL–DTL– 5015 S III
MIL-DTL-5015 Series III, Rear Release
Flange and Jam Nut Receptacles
Panel Cutouts
Panel Cutouts
– –
A
[ C[ B
E
[ D
.100(2.54) DIA.
.095(2.41)
MS3454 (AE554) CUTOUT
Flange and Jam Nut Mounting Dimensions
Shell
Size
A⭋B⭋C ⭋D E
Classes L, LS, W Classes KS, KT
+.010 +.25 +.010 +.25 +.015 +.38
(TP) ±.010 ±.25 -.005 -.13 -.005 -.13 -.000 -.00 ±.005 ±.13
inch mm inch mm inch mm inch mm inch mm inch mm
8S .594 15.09 .562 14.27 .120 3.05 .150 3.81 .505 12.83 .323 8.20
10S, 10SL .719 18.26 .688 17.48 .120 3.05 .150 3.81 .630 16.00 .385 9.78
12, 12S .812 20.62 .812 20.62 .120 3.05 .150 3.81 .755 19.18 .448 11.38
14, 14S .906 23.01 .938 23.83 .120 3.05 .150 3.81 .880 22.35 .510 12.95
16, 16S .969 24.61 1.062 26.97 .120 3.05 .150 3.81 1.005 25.53 .573 14.55
18 1.062 26.97 1.188 30.18 .120 3.05 .177 4.50 1.130 28.70 .635 16.13
20 1.156 29.36 1.312 33.32 .120 3.05 .177 4.50 1.255 31.88 .698 17.73
22 1.250 31.75 1.438 36.53 .120 3.05 .177 4.50 1.380 35.05 .760 19.30
24 1.375 34.93 1.562 39.67 .147 3.73 .177 4.50 1.505 38.23 .823 20.90
28 1.562 39.67 1.812 46.02 .147 3.73 .177 4.50 1.755 44.58 .948 24.08
32 1.750 44.45 2.062 52.37 .173 4.39 .209 5.31 2.005 50.93 1.073 27.25
36 1.938 49.23 2.312 58.72 .173 4.39 .209 5.31 2.255 57.28 1.198 30.43
40 2.188 55.58 2.562 65.07 .173 4.39 .209 5.31 2.505 63.63 1.323 33.60
56www.conesys.com sales@aero-electric.com
MIL–DTL– 5015 S III
MIL-DTL-5015
Contacts, Tools and Seal Plugs
MS345*/AE55*
Contacts, Plastic Insertion/Removal Tools and Seal Plugs
Crimping and Metal Insertion/Extraction Tools
Contact and Wire Data
– –
† MS3348 bushings required in crimp barrel to accommodate 10, 6 and
2 wire gauges. Bushings are ordered separately.
Note 1: 16S socket contacts are only used in shell sizes 8S,
10S, 10SL, 12S, 14S and 16S.
Note 2: Test Current and Maximum Voltage Drop when
tested with silver-plated wire at 25°C.
* No spare size 0, 4 and 8 contacts are provided in connector contact packages.
** Not supplied as part of connector contact packages.
Note 3: Metal Insertion tool is not req’d for size 8, 4
and 0 contacts. Metal insertion tool for size 16 contacts =
M81969/8-207. Metal insertion tool for size 12 contacts =
M81969/8-209.
Contact
Size
Application Pin Contacts Socket Contacts Seal Plugs Insertion/Removal Tools
Plastic
Type Military No. Military No. Military No. Military No.
16S Power/Signal N/A M39029/30-217 MS27488-16-1 M81969/14-03
16 Power/Signal M39029/29-212 M39029/30-218
12 Power/Signal M39029/29-213 M39029/30-219 MS27488-12-1 M81969/14-04
8 Power M39029/29-214* M39029/30-220* MS27488-8-1 M81969/14-06
4 Power M39029/29-215* M39029/30-221* MS27488-4-1** M81969/14-07
0 Power M39029/29-216* M39029/30-222* MS27488-0-1** M81969/14- 08
Contact
Size
Crimp Tool Positioner Die Set Locator Extraction Tool
Pin & Socket Contacts Pin & Socket Contacts Pin & Socket Contacts Metal
Military No. Military No. Military No. Military No. Military No.
16/16S M22520/1-01 M22520/1-02 N/A N/A M81969/8-208
12 M22520/1-01 M22520/1-02 N/A N/A M81969/8-210
8 M22520/23-01 N/A M22520/23-02 M22520/23-09 M81969/15-01
4 M22520/23-01 N/A M22520/23-03 M22520/23-11 M81969/15- 02
0 M22520/23-01 N/A M22520/23-04 M22520/23-13 M81969/15- 03
Contact
Size
Test Current Voltage Crimp Well Data Wire Range Finished Wire ⭋Range
DC Test Max. Drop Well Dia. Minimum Well Dept Minimum Maximum
Amps Millivolts inch inch mm AWG mm2inch mm inch mm
16/16S 13 49 .067 ±.001 .250 6.35 20-16 0.52-1.31 .053 1.35 .103 2.62
12 23 42 .100 ±.002 .250 6.35 14-12 2.08-3.31 .085 2.16 .158 4.01
8 46 26 .181 ±.002 .485 12.32 10-8† 5.26-8.37 .132 3.35 .255 6.48
4 80 23 .281 ±.002 .485 12.32 6-4† 13.30-21.15 .237 6.02 .370 9.40
0 150 21 .453 ±.002 .580 14.73 2-0† 33.63-53.48 .360 9.14 .550 13.97
57www.conesys.com sales@aero-electric.com
MIL–DTL– 5015 S III
MIL-DTL-5015
Contact Installation Instructions
MS345*/AE55*
– –
Contact Installation
Instructions
Crimping Contacts
1. Select the appropriate crimp tool and ensure that the
proper crimp head positioner is used.
2. Cycle the tool to be sure the indentors are open.
3. Determine the correct selector setting for the wire size
from the data plate on the positioner (turret head
assembly) and set the selector knob on the crimp tool
to match.
4. Place the contact, mating end first, into the tool.
5. Insert the stripped wire into the hollow end of the
contact. Be sure the wire is inserted as far as it will go.
6. Close the tool completely to crimp. Unless the tool is
closed completely, the tool will not release the contact.
7. Remove the crimped contact from the tool. Check the
inspection hole to verify that the wire is fully inserted.
Insertion of Contacts
1. Before inserting the contacts, unscrew the accessories
(clamps, backshells or adapters) from rear of plug or
receptacle. Slide the hardware over the wire bundle in
the proper order for reassembly after all the contacts
are inserted.
2. To assist insertion of contacts, lubricate insulator
(grommet) cavities with isopropyl alcohol. Alcohol will
evaporate and will not leave a conductive film. Caution:
Never use any lubricant other than isopropyl alcohol.
3. Place the correct insertion tool on the contact so that the
wire runs along the groove in the tool. (Tool tip will butt
against the shoulder.) Hold the plug or receptacle body
firmly.
4. Beginning with a center cavity, insert the contact into
the insulator with a slow, even pressure until the contact
snaps into position. Make sure the contact and tool are
held perpendicular to the face of the insert during the
contact installation or the grommet could be damaged.
4.1 If contacts are not inserted all the way prior to
removing insertion tool, do not try to reinsert the
insertion tool. Instead, remove the contact and try
again; otherwise reinserting the insertion tool may
damage the inside of the contact cavity.
5. Remove tool and check the face of the connector for
proper contact installation. Proper installation may also
be checked by pulling back lightly on the wire to make
sure the contact is properly seated.
Completion
After all the cavities have been filled, slide the hardware back
into position on the connector and tighten.
Extraction of Contacts (Rework)
1. Slide the hardware back over the wire bundle.
2. Select the appropriate tool. Place the wire into the
extraction tool of the pin or socket.
3. Slowly slide the extraction tool down wire into the contact
cavities until the tool tip bottoms against the contact
shoulder, expanding the clip retaining tines. Hold the
wire firmly in the tool and pull the wired contact and
tool straight out of the rear of the insulator.
I/R = Insertion/Removal
* 16S socket contact is only used in shell sizes 8S, 10S, 10SL, 12S, 14S and 16S.
Size Pin Contact Socket Contact Crimp Tool Positioner Die Set Locator I/R Tool
16S* — M39029/30-217 M22520/1-01 M22520/1-02 Blue — — M81969/14-03
16 M39029/29-212 M39029/30-218 M22520/1-01 M22520/1-02 Blue — — M81969/14-03
12 M39029/29-213 M39029/30-219 M22520/1-01 M22520/1-02 Yellow — — M81969/14-04
8 M39029/29-214 M39029/30-220 M22520/23-01 — M22520/23-02 M22520/23-09 M81969/14-06
4 M39029/29-215 M39029/30-221 M22520/23-01 — M22520/23-04 M22520/23-11 M81969/14-07
0 M39029/29-216 M39029/30-222 M22520/23-01 — M22520/23-05 M22520/23-13 M81969/14-08
58www.conesys.com sales@aero-electric.com
MIL–DTL– 5015 S III
MIL-DTL-5015 Series III (Rear Release)
Polarization, Insert Availability & Contact Information
per MIL-STD-1651
Insert Availability, Contact Information and Clocking Positions
– –
Polarization (Insert Clocking)
1. In the normal insert clocking position (position N),
the insert centerline coincides with the centerline of the
master keyway (key) of the shell: L = 0°.
2. In the alternate clocking positions (W, X, Y and Z),
the pin insert (viewing from mating side) is rotated
clockwise relative to the centerline of the master
keyway (key) of the shell.
3. The socket insert is rotated counter-clockwise.
4. Plugs have keyways; receptacles have keys.
Note: Be careful with alternate positions. See table below for
position availability on layouts of interest.
* Inactive for new design
** Pin contact is size 16, socket contact is size 16S
*** Service Rating = Inst. for classes KS and KT only.
Shell Size
& Insert
Arrangement
Aero-Electric Contacts Insert Positions
Status Total Quantity by Size Service Contact “L” Degrees
QPL’d Tooled Number Qty Size Rating Location N W X Y Z
8S-1 Yes Yes 1 1 16/16S** A All 0 — — — —
10S-2 Yes Yes 1 1 16/16S** A All 0 — — — —
10SL-3*** Yes Yes 3 3 16/16S** A All 0 — — — —
10SL-4 Yes Yes 2 2 16/16S** A All 0 — — — —
12-5 Yes Yes 1 1 12 D All 0 — — — —
12S-3 Yes Yes 2 2 16/16S** A All 0 70 145 215 290
12S-4 Yes Yes 1 1 16/16S** D All 0 — — — —
14-3 Yes Yes 1 1 8 A All 0 — — — —
14S-1* Yes Yes 3 3 16/16S** A All 0 — — — —
14S-2 Yes Yes 4 4 16/16S** Inst. All 0 — 120 240 —
14S-5 Yes Yes 5 5 16/16S** Inst. All 0 — 110 — —
14S-6 Yes Yes 6 6 16/16S** Inst. All 0 — — — —
14S-7 Yes Yes 3 3 16/16S** A All 0 90 180 270 —
14S-9* Yes Yes 2 2 16/16S** A All 0 70 145 215 290
16-10 Yes Yes 3 3 12 A All 0 90 180 270 —
16-11 Yes Yes 2 2 12 A All 0 35 110 250 325
16-12 Yes Yes 1 1 4 A All 0 — — — —
16S-1 Yes Yes 7 7 16/16S** A All 0 80 — — 280
16S-4 Yes Yes 2 2 16/16S** D All 0 35 110 250 325
16S-5* Yes Yes 3 3 16/16S** A All 0 70 145 215 290
16S-8 Yes Yes 5 5 16/16S** A All 0 — 170 265 —
PIN INSERT
MATING FACE
(SOCKET INSERT IS OPPOSITE)
INSERT
VERTICAL
CENTERLINE
MASTER
KEYWAY(KEY)
OF A SHELL
L°
59www.conesys.com sales@aero-electric.com
MIL–DTL– 5015 S III
MIL-DTL-5015 Series III (Rear Release)
Insert Availability, Contact Information and Clocking
per MIL-STD-1651
Insert Availability, Contact Information and Clocking Positions
– –
Shell Size
& Insert
Arrangement
Aero-Electric Contacts Insert Positions
Status Total Quantity by Size Service Contact “L” Degrees
QPL’d Tooled Number Qty Size Rating Location N W X Y Z
18-1 Yes Yes 10 4 16 A B,C,F,G 0 70 145 215 290
6 16 Inst. All others
18-4 Yes Yes 4 4 16 D All 0 35 110 250 325
18-5 Yes Yes 31 16 D All 0 80 110 250 280
2 12
18-6 Yes Yes 1 1 4 D — 0 — — — —
18-8 Yes Yes 87 16 A All 0 70 — — 290
1 12
18-9 Yes Yes 75 16 Inst. All 0 80 110 250 280
2 12
18-10* Yes Yes 4 4 12 A All 0 — 120 240 —
18-11 Yes Yes 5 5 12 A All 0 — 170 265 —
18-12 Yes Yes 6 6 16 A All 0 80 — — 280
18-20* Yes Yes 5 5 16 A All 0 90 180 270 —
20-2 Yes Yes 1 1 0 D --- 0 — — — —
20-3* Yes Yes 3 3 12 D All 0 70 145 215 290
20-4 Yes Yes 4 4 12 D All 0 45 110 250 —
20-7 Yes Yes 84 16 D A,B,G,H 0 80 110 250 280
4 16 A All others
20-8 Yes Yes 64 16 Inst. All 0 80 110 250 280
2 8
20-11* Yes Yes 13 13 16 Inst. All 0 — — — —
20-14 Yes Yes 53 12 A All 0 80 110 250 280
2 8
20-15 Yes Yes 7 7 12 A All 0 80 — — 280
20-16 Yes Yes 97 16 A All 0 80 110 250 280
2 12
20-17 Yes Yes 61 16 A All 0 90 180 270 —
5 12
20-18 Yes Yes 96 16 A All 0 35 110 250 325
3 12
20-22 Yes Yes 63 16 A All 0 80 110 250 280
3 8
20-24* Yes Yes 42 16 A All 0 35 110 250 325
2 8
20-27 Yes Yes 14 14 16 A All 0 35 110 250 325
20-29 Yes Yes 17 17 16 A All 0 80 — — 280
20-33 Yes Yes 11 11 16 A All 0 — — — —
22-1* Yes Yes 2 2 8 D All 0 35 110 250 325
* Inactive for new design
60www.conesys.com sales@aero-electric.com
MIL–DTL– 5015 S III
MIL-DTL-5015 Series III (Rear Release)
Insert Availability, Contact Information and Clocking
per MIL-STD-1651
Insert Availability, Contact Information and Clocking Positions
– –
* Inactive for new design
** Alternate positions X, Y are cancelled after June 26, 1968.
Shell Size &
Insert
Arrangement
Aero-Electric Contacts Insert Positions
Status Total Quantity by Size Service Contact “L” Degrees
QPL’d Tooled Number Qty Size Rating Location N W X Y Z
22-2 Yes Yes 3 3 8 D All 0 70 145 215 290
22-9 Yes Yes 3 3 12 E All 0 70 145 215 290
22-12 Yes Yes 53 16 D All 0 80 110 250 280
2 8
22-13* Yes Yes 51 16 D E 0 35 110 250 325
4 12 A All others
22-14** Yes Yes 19 19 16 A All 0 80 110 250 280
22-18 Yes Yes 83 16 A C,D,E 0 80 110 250 280
5 16 D All others
22-19 Yes Yes 14 14 16 A All 0 80 110 250 280
22-20* Yes Yes 9 9 16 A All 0 35 110 250 325
22-22 Yes Yes 4 4 8 A All 0 — 110 250 —
22-23 Yes Yes 81 12 D H 0 35 — 250 —
7 12 A All others
22-27 Yes Yes 91 8 D J 0 80 — 250 280
8 16 A All others
22-33* Yes Yes 73 16 A E,F,G 0 80 110 250 280
4 16 D All others
24-2 Yes Yes 7 7 12 D All 0 80 — — 280
24-4 Yes Yes 43 16 D All 0 80 110 250 280
1 0
24-6 Yes Yes 83 12 D A,G,H 0 80 110 250 280
5 12 A All others
24-7 Yes Yes 16 14 16 A All 0 80 110 250 280
2 12
24-9* Yes Yes 2 2 4 A All 0 35 110 250 325
24-10 Yes Yes 7 7 8 A All 0 80 — — 280
24-11 Yes Yes 96 12 A All 0 35 110 250 325
3 8
24-12 Yes Yes 53 12 A All 0 80 110 250 280
2 4
24-20 Yes Yes 11 9 16 D All 0 80 110 250 280
2 12
24-21 Yes Yes 10 9 16 D All 0 80 110 250 280
1 8
24-22 Yes Yes 4 4 8 D All 0 45 110 250 —
24-27 Yes Yes 7 7 16 E All 0 80 — — 280
24-28 Yes Yes 24 24 16 Inst. All 0 80 110 250 280
61www.conesys.com sales@aero-electric.com
MIL–DTL– 5015 S III
MIL-DTL-5015 Series III (Rear Release)
Insert Availability, Contact Information and Clocking
per MIL-STD-1651
Insert Availability, Contact Information and Clocking Positions
– –
* Inactive for new design
Shell Size &
Insert
Arrangement
Aero-Electric Contacts Insert Positions
Status Total Quantity by Size Service Contact “L” Degrees
QPL’d Tooled Number Qty Size Rating Location N W X Y Z
28-1 Yes Yes 9
2 12 D A,E
0 80 110 250 280
4 12 A B,D,F,H
1 8 D J
2 8 A G,C
28-2 Yes Yes 14 12 16 D All 0 35 110 250 325
2 12
28-3 Yes Yes 3 3 8 E All 0 70 145 215 290
28-5 Yes Yes 5
2 16
D All 0 35 110 250 3251 12
2 4
28-8 Yes Yes 12
2 12 E L,M
1 16 D B 0 80 110 250 280
9 16 A All others
28-9 Yes Yes 12 6 16 D All 0 80 110 250 280
6 12
28-11 Yes Yes 22 18 16 A All 0 80 110 250 280
4 12
28-12 Yes Yes 26 26 16 A All 0 90 180 270 —
28-15 Yes Yes 35 35 16 A All 0 80 110 250 280
28-16* Yes Yes 20 20 16 A All 0 80 110 250 280
28-19 Yes Yes 10
2 16 B H,M
0 80 110 250 280
2 16 D A,B
2 16 A All others
4 12
28-20 Yes Yes 14 4 16 A All 0 80 110 250 280
10 12
28-21 Yes Yes 37 37 16 A All 0 80 110 250 280
28-22 Yes Yes 63 16 D All 0 70 145 215 290
3 4
32-1 Yes Yes 5
1 12 E A
0 80 110 250 2802 12 DD,C
2 0 B,E
32-3 Yes Yes 9
4 16
D All 0 80 110 250 280
2 12
2 4
1 0
32-5* Yes Yes 2 2 0 D All 0 80 110 250 325
32-6 Yes Yes 23
16 16
A All 0 80 110 250 280
2 12
3 8
2 4
62www.conesys.com sales@aero-electric.com
MIL–DTL– 5015 S III
MIL-DTL-5015 Series III (Rear Release)
Insert Availability, Contact Information and Clocking
per MIL-STD-1651
Insert Availability, Contact Information and Clocking Positions
– –
* Inactive for new design
** Alternate positions U (100 degrees) and V (260 degrees) are also
available per MIL-STD-1651.
Shell Size
& Insert
Arrangement
Aero-Electric Contacts Insert Positions
Status Total Quantity by Size Service Contact “L” Degrees
QPL’d Tooled Number Qty Size Rating Location N W X Y Z
32-7 Yes Yes 35
4 16 Inst. A,B,h,j
0 80 125 235 28024 16 A All others
7 12
32-8* Yes Yes 30 24 16 A All 0 80 125 235 280
6 12
32-10* Yes Yes 7
2 16 E A,F
0 80 110 250 280
1 16 B G
2 8 D B,E
2 4 A C,D
32-15 Yes Yes 86 12 D All 0 35 110 250 280
2 0
32-17 Yes Yes 4 4 4 D All 0 45 110 250 ---
32-22** Yes Yes 54 54 16 A All 0 80 110 250 280
32-63 Yes Yes 5 5 4 D All 0 — — — —
32-73 Yes Yes 46 46 16 A All 0 36 — — —
36-3 Yes Yes 63 12 D All 0 70 145 215 290
3 0
36-5 Yes Yes 4 4 0 A All 0 — 120 240 —
36-6 Yes Yes 64 4 A All 0 35 110 250 325
2 0
36-7 Yes Yes 47 40 16 A All 0 80 110 250 280
7 12
36-8 Yes Yes 47 46 16 A All 0 80 110 250 280
1 12
36-9 Yes Yes 31
14 16
A All 0 80 125 235 280
14 12
2 8
1 4
36-10 Yes Yes 48 48 16 A All 0 80 125 235 280
40-10 Yes Yes 29
16 16
A All 0 65 125 225 3109 8
4 4
40-56 Yes Yes 85 85 16 A All 0 72 144 216 288
63www.conesys.com sales@aero-electric.com
MIL–DTL– 5015 S III
MIL-STD-1651
Insert Arrangements (Pin Front View)
for MIL-DTL-5015 Connectors
Insert Arrangement Views
– –
* Inactive for new design
64www.conesys.com sales@aero-electric.com
MIL–DTL– 5015 S III
MIL-STD-1651
Insert Arrangements (Pin Front View)
for MIL-DTL-5015 Connectors
Insert Arrangement Views
– –
20-15
7- #12
20-24*
2- #16, 2- #8
A
B
C
D
E
F
G
H
J
K
L
M
N
I
20-27
14- #16
A
B
C
D
E
T
F
G
H
J
K
L
M
N
P
R
S
20-29
17- #16
A
B
C
D
E
F
H
J
K
L
M
20-33
11- #16
20-16
7- #16, 2- #12
20-17
1- #16, 5- #12
20-18
6- #16, 3- #12
20-22
3- #16, 3- #8
A
B
22-1*
2- #8
22-2
3- #8
A
B
C
D
E
F
G
H
I
A
B
C
D
E
F
G
A
B
C
D
E
F
A
B
CDE
F
G H
I
A
B
C
D
E
F
A
B
C
D
A
B
C
A
B
C
22-9
3- #12
22-12
3- #16, 2- #8
A
B
C
D
E
22-13*
1- #16, 4- #12
A
B
C
D
E
A
B
C
D
E
F
G
H
J
K
L M
N
P
R
S
V
U
T
22-14
19- #16
A
B
C
D
E
G
H
F
A
B
C
D
20-4
4- #12
20-7
8- #16
A
B
C
D
E
F
20-8
4- #16, 2- #8
A
BC
D
EF
GH
J
K
L
M
N
20-11*
13- #16
A
B
C
D
E
20-14
3- #12, 2- #8
* Inactive for new design
65www.conesys.com sales@aero-electric.com
MIL–DTL– 5015 S III
MIL-STD-1651
Insert Arrangements (Pin Front View)
for MIL-DTL-5015 Connectors
Insert Arrangement Views
– –
A
B
A
B
C
D
E
F
G
A
B
C
D
E
F
H
JK
G
A
B
C
D
A
B
C
D
E
F
G
A
B
C
D
J
E F H
K
L M N P Q
RSTUV
W X Y Z
G
24-7
14- #16, 2- #12
24-9*
2- #4
24-10
7- #8
24-11
6- #12, 3- #8
24-12
3- #12, 2- #4
24-20
9- #16, 2- #12
24-21
9- #16, 1- #8
24-22
4- #8
24-27
7- #16
24-28
24- #16
A
B
C
L
D
E
F
H
G
J
K
A
B
C
D E F
HI
G
A
B
C
D
E
A
B
C
D
E
F
G
H
I
J
K
L
M
N
O
P
B
A
C
D
E
F
G
H
22-18
8- #16
A
B
J
C
D
E
F
G
HA
B
C
D
E
F
G
22-27
1- #8, 8- #16
22-33*
7- #16
A
B
C
D
E
F
G
H
J
K
L
M
N
P
22-19
14- #16
A
B
C
DE
F
GH
J
22-20*
9- #16
A
B
C
D
22-22
4- #8
A
B
C
D
E
F
G
H
22-23
8- #12
A
B
C
D
E
F
G
24-2
7- #12
A
B
C
D
24-4
3- #16, 1- #0
A
B
C
D
E
F
H
G
24-6
8- #12
* Inactive for new design
66www.conesys.com sales@aero-electric.com
MIL–DTL– 5015 S III
MIL-STD-1651
Insert Arrangements (Pin Front View)
for MIL-DTL-5015 Connectors
Insert Arrangement Views
– –
28-1
6- #12, 3- #8
28-2
12- #16, 2- #12
28-3
3- #8
28-5
2- #16, 1- #12, 2- #4
28-8
2- #12, 10- #16 28-9
6- #16, 6- #12
28-11
18- #16, 4- #12
28-12
26- #16
28-15
35- #16
28-16*
20- #16
28-19
6- #16, 4- #12
28-20
4- #16, 10- #12
28-21
37- #16
28-22
3- #16, 3- #4
32-1
3- #12, 2- #0
A
P
B
C
D
E
F
G
H
J
K
L
M
N
A
B
C
DEF
H
J
G
A
B
C
A
B
C
D
E
A
B
C
D
E
F
G
H
J
K
L
M
A
B
C
D
E
F
G
H
J
K
L
M
A
B
C
D
E
F
G
H
I
J
K
L
M
N
P
R
S
T
U
V
W
X
A
B
C
D
E
F
G
H
J
K
L
M
N
P
R
S
T
U
V
W
X
Y
Z
a
b
d
A
a b c
defgh
l
jk
m
B
CD E F G
HJK L M N
P R STUV W
X Y Z
A B
C
D
EF
G
H
J
K
L M
N
P
Q
R
S
T
U
V
AB
C
E
G
H
J
K
L
M
A
B
C
D
E
F
G
H
J
K
L
M
N
P
A B CD
E F GHJ
K L M N P R
STUV W X Z
a b
c
def
ghjk m
n
pr
s
A
B
C
D
E
FA
B
C
D
E
32-3
4- #16, 2- #12,
2- #4, 1- #0
ABC
D
E
F
G
H
J
* Inactive for new design
67www.conesys.com sales@aero-electric.com
MIL–DTL– 5015 S III
MIL-STD-1651
Insert Arrangements (Pin Front View)
for MIL-DTL-5015 Connectors
Insert Arrangement Views
– –
32-5*
2- #0
32-7
28- #16, 7- #12
32-8*
24- #16, 6- #12
32-10*
3- #16, 2- #8,
2- #4
32-15
6- #12, 2- #0
32-17
4- #4
32-22
54- #16
32-63
5- #4
32-73
46- #16
36-3
3- #12, 3- #0
36-5
4- #0
A
B
32-6
16- #16, 2- #12,
3- #8, 2- #4
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
A
B
C
D
A
B
C
D
E
F
A
BC
DE
F
G
H
A
B
C
D
E
A
B
C
D
A
B
C
D
G
F
E
AB
CD
EF
G
H
IJ
K
LM
N
P
ORS
T
UV
WX
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
C D E
FG H J
XY
KLM
N P RO
S
TUVW
Za
bc d e f
ghjk
mnpqr
y
st u v
wx
zAA
AB
AC
AD
AF AG
AE
1
2
3
4
5
6
7
8
9
10
11
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
* Inactive for new design
68www.conesys.com sales@aero-electric.com
MIL–DTL– 5015 S III
MIL-STD-1651
Insert Arrangements (Pin Front View)
for MIL-DTL-5015 Connectors
Insert Arrangement Views
– –
36-9
14- #16, 14- #12,
2- #8, 1- #4
36-10
48- #16 40-10
16- #16, 9- #8,
4- #4
40-56
85- #16
A
B
C
D
E
H
F
G
I
J
K
L
M
N
O
P
R
S
T
U
V
W
X
Y
Z
a
b
c
d
e
f
A B
CD E F G
HJK L M N
OPQRSTU
V W X Y Z
a
bc
defghjk
m n pqrs
tuvw x
yz
A
B
CD
E
F
GH
I
JK
L
MNOPQ
R
ST
U
VWX
Y
Za
b
c
A
BCD
E F H JK L M
N P R STUV W
X Y Z a b cdfg
hjki m n p q rs
tuv w x yz AA AB
AC AD AE AF AH AJ AK AL AM AN
AP AR AS AT AU AV AW AX AY
AZ BA BB BC BD BE BF BH
BJ BK BL BM BN BP BR
BS BT BU BV
36-6
4- #4, 2- #0
36-7
40- #16, 7- #12
36-8
46- #16, 1- #12
A
B
C
D
E
F
AB
CDE
FG
HIJ
KLMN
OPR S T
UVWX
YZabc
m
de f g
hjt
k
np
uwv
rs
xzy
A
B
C
DE
F
GH
IJKL
M
NOPR
STUV
WXYZa
bcde
fgh
y
j
k
w
mn
x
p
z
r
st
u
v