MIL-DTL-38999 Features and Application Series III Features and Application Universal I/R Tool - A single, expendable plastic tool is used for both insertion and removal of contacts. Scoop-Proof Design - Recessed pins in elongated shells minimize the possibility for contact damage. In a blind mating application, mating shells cannot "scoop" the pins, and cause a shorting or bending of contacts. MIL-DTL-38999 Series III is the newest cylindrical connector designed for highest performance capabilities used in both general purpose and severe environment applications. MIL-DTL- 38999 S III These connectors feature an improved "one-turn" coupling system, utilizing self-locking acme thread. Acme threads provide coupling durability, while thicker wall sections and greater coupling surface area improve strength and shock resistance. Blunting of the threads on both receptacle and plug coupling nut eliminates cross threading. 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. Elongated mounting holes permit the Series III Connector to intermount with various existing Mil-spec flange mounted receptacles, giving it a design replacement advantage. 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. Wall mount receptacle, jam nut receptacle and straight self-locking RFI plug are offered in 9 shell sizes and 54 insert arrangements utilizing M39029 contacts in sizes 22D, 20, 16, 12, 10 power and 8 twinax. 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. These connectors are available in wide range of shell materials and finishes. Aluminum shells are offered in electroless nickel and olive drab cadmium. Other finishes such as anodic and zinc nickel are available upon request to commercial callouts only. In addition, we offer stainless steel shells (both passivated and electro-deposited nickel plated) with firewall inserts, and for highly corrosive environments, nickel-aluminum-bronze shells with standard environment-resisting inserts (commercial callouts only). Metric Accessory Thread - Metric thread results in additional wall thickness giving greater strength and shock resistance. MIL-STD-1560 Insert Arrangements - Series III connectors use insert patterns and contacts common to Series I, making for an easy transition from bayonet to triple-lead, acme-thread, self-locking coupling. Metal-to-Metal Bottoming - This feature precludes relative shell-to-shell motion, which may result in ordinary connector wear and moisture entrapment. Lockwiring Eliminated - Self-locking quick coupling plug eliminates the need for lockwiring. Firewall Capability - Stainless steel shells in both K and S firewall classes are offered. www.conesys.com - 36 - sales@aero-electric.com MIL-DTL-38999 Performance Specifications Series III Performance Specifications Environmental Seal Wired, mated connectors with specified accessories attached, shall meet the altitude-immersion test specified in MIL-DTL-38999. Operating Temperature Range Classes F, K, S and BZ*: -65C to +200C (-85F to +392F) Classes W and ZC*: -65C to +175C (-85F to +347F) Shell-to-Shell Conductivity Maximum potential drop shall not exceed: Classes F and S = 1.0 millivolt. Class W = 2.5 millivolts, Class K = 10.0 millivolts Shock and Vibration Requirements Wired, mated connectors shall not be damaged, nor shall there be a current interruption longer than one microsecond when subjected to the following: Corrosion Resistance Classes K, W, BZ* and Z* withstand 500-hour salt spray. Classes F and S withstand 48-hour salt spray. Shock Pulse of approximate half sine wave of 300 G 15 percent magnitude with duration of 3 1 milliseconds applied in three axes. Durability Minimum of 500 mating cycles. High Impact Shock When mounted as specified in MIL-S-901, grade A, a drop of a 400 lb. Hammer from 1 foot, 3 feet and 5 feet applied to connector in three axes, totaling nine impacts. Fluid Resistance Connectors resist specified immersions in MIL-PRF-7808, MIL-PRF-23699, MIL-PRF-5606, M2-V Chevron oil, Coolanol 25, MIL-DTL-83133 (JP-8), MIL-DTL-5624 (JP-4, JP-5), SAE-AMS1424 Type I, and other solvents and cleaning agents. Shielding Effectiveness RFI and EMI attenuation at the specified frequencies meet the requirements of MIL-DTL-38999. RFI shielding effectiveness of mated connectors with RFI backshells is measured in a triaxial radio frequency leakage fixture. EMI shielding effectiveness is measured at the interface of mated connectors and tested by the mode-stirred technique specified in method 3008 of MIL-STD-1344. Vibration Wired and mated connectors withstand the following vibration levels: Sine vibration where connector samples with simulated accessory load are subjected to simple harmonic motion from 10 to 2,000 Hz in three mutually perpendicular axes, in 20 minute sweeps, for 12 hours in each axis at velocity of 254 mm/sec from 10-50 Hz, displacement of 1.5 mm from 50-140Hz and acceleration of 60G from 140-2,000Hz. Random Vibration per MIL-STD-1344, method 205, test condition V at ambient temperature and test condition VI, Letter "J" at elevated temperature. Voltage Rating * Not on QPL, can be supplied to Aero-Electric part number only. Service Rating M N I II Suggested Operating Voltage Test Voltage Test Voltage Test Voltage Test Voltage (Sea Level) Sea Level V RMS 1300 1000 1800 2300 50,000 Ft. V RMS 550 400 600 800 70,000 Ft. V RMS 350 260 400 500 100,000 Ft. V RMS 200 200 200 200 AC (RMS) 400 300 600 900 DC 550 450 850 1250 Note: The establishment of electrical safety factors is left entirely to the designer, as he is in the best position to know www.conesys.com exactly what peak voltages, switching currents, transients, etc., can be expected in a particular circuit. - 37 - sales@aero-electric.com MIL-DTL- 38999 S III Material and Finish Data (Class) F - aluminum shell, electroless nickel finish K - stainless steel shell, passivated, firewall S - stainless steel shell, electrodeposited nickel, firewall W- aluminum shell, olive drab cadmium over nickel base BZ* - aluminum nickel bronze shell, std insert Z*- aluminum shell, zinc nickel finish MIL-DTL-38999 Part Number Development Series III Military and Aero-Electric Part Number Development Mil. Prefix Aero Prefix D38999/ AE3 20 20 W W C C 35 35 P P N N -340 Shell Type (Specification Sheet Number) 20 = Wall mount receptacle 24 = Jam nut receptacle 26 = Self-locking, RFI grounding plug MIL-DTL- 38999 S III Class (Material & Finish) F = Aluminum shell, electroless nickel finish W = Aluminum shell, olive drab cadmium over electroless nickel base K = Stainless steel shell, passivated, with firewall insert S = Stainless steel shell, electrodeposited nickel, with firewall insert BZ* = Aluminum nickel bronze shell with standard insert (Aero p/n only) Z* = Aluminum shell, zinc nickel plating (Aero p/n only) Shell Size A, B, C, D, E, F, G, H or J Insert Arrangement See pages 15 thru 19 Contact Style P = Pin S = Socket A = Pin connector less pins (with intent to use non-std pin contacts) B = Socket connector less sockets (with intent to use non-std socket contacts) Polarization (Keying) N = Normal (Included in part number) A, B, C, D, or E Modification (applies to Aero part numbers only) 01 = Less contacts (is not marked on the part) 340 = Connector kitted with M85049/14-XXX 341 = Connector kitted with M85049/38-XXX straight clamp 342 = Connector kitted with M85049/39-XXX right angle clamp Consult factory for other modifications * Not on QPL, can be supplied to Aero-Electric part number only. Note 1: Each connector is furnished with contacts unless ordered less contacts (L/C) as follows: One spare contact for inserts requiring 2 through 26 of each contact and two spares for inserts with 27 or more contacts, and a minimum of one sealing plug up to 10% of the number contacts. Spare Coax and Twinax contacts are not supplied. One insertion/extraction tool for each contact size is also included. www.conesys.com Note 2: Proper part number marking has no "0" in front of single digit layout. Example: JD38999/20WB5SN. "N" for normal is included. In addition, J or JAN must be marked immediately in front of MIL part number. - 38 - sales@aero-electric.com D38999/20 Wall Mounting Receptacle AE320 Triple Start Threaded Coupling, Crimp Removable, Rear Release, Scoop-Proof 31.50(1.240) MAX A G MASTER KEYWAY H MAX MAX 7.11(.280) MIN FULL THREAD 2.16(.085) MAX GROMMET EXTENSION D [L MIL-DTL- 38999 S III MAX GROMMET J NUMBER OF TEETH F E MATING THREAD 4 MINOR KEYWAYS K ACCESSORY THREAD LOCKING INDICATOR BAND COLOR: RED C BLUE COLOR BAND (REAR RELEASE) B Page 38 Page 44 Pages 17-19 Page 37 Pages 15, 16 Page 42 Note 1: "K" Accessory Thread for AE320 is same as AE326 ("D" Accessory Thread) on page 41. Completed Part Number Contacts, Sealing Plugs and Tools Insert Arrangements Performance Specifications Insert Availability and Contact Information Polarization Note 2: "F" Mating Thread for AE320 is same as AE326 ("E" Mating Thread) on page 41 except it is Class 2A. Note 3: Maximum Grommet Extension for insert layouts incorporating size 8 and 10 contacts = 5.95(.234). A B C (TP) (TP) Shell Size .012 .30 inch mm inch mm inch A .937 23.80 .719 18.26 B 1.031 26.20 .812 D E G H J Maximum Maximum No. of Teeth .008 .20 .008 .20 mm inch mm inch mm inch mm inch mm .594 15.09 .216 5.49 .128 3.25 .820 20.83 .098 2.50 20.62 .719 18.26 .194 4.93 .128 3.25 .820 20.83 .098 L Maximum inch mm 12 .299 7.59 2.50 16 .427 10.85 C 1.126 28.60 .906 23.01 .812 20.62 .194 4.93 .128 3.25 .820 20.83 .098 2.50 20 .541 13.74 D 1.220 31.00 .969 24.61 .906 23.01 .173 4.39 .128 3.25 .820 20.83 .098 2.50 24 .666 16.92 E 1.311 33.30 1.062 26.97 .969 24.61 .194 4.93 .128 3.25 .820 20.83 .098 2.50 28 .791 20.09 F 1.437 36.50 1.156 29.36 1.062 26.97 .194 4.93 .128 3.25 .820 20.83 .098 2.50 32 .897 22.78 G 1.563 39.70 1.250 31.75 1.156 29.36 .194 4.93 .128 3.25 .790 20.07 .126 3.20 36 1.022 25.96 H 1.689 42.90 1.375 34.93 1.250 31.75 .242 6.15 .154 3.91 .790 20.07 .126 3.20 40 1.147 29.13 J 1.811 46.00 1.500 38.10 1.375 34.93 .242 6.15 .154 3.91 .790 20.07 .126 3.20 44 1.272 32.31 www.conesys.com - 39 - sales@aero-electric.com D38999/24 Jam Nut Receptacle AE324 Triple Start Threaded Coupling, Crimp Removable, Rear Release, Scoop-Proof A D 32.50 (1.280) MAX BLUE COLOR BAND (REAR RELEASE) G LOCKING INDICATOR BAND COLOR: RED MASTER KEYWAY 2.16(.085) MAX GROMMET EXTENSION [H B MAX GROMMET MIL-DTL- 38999 S III FLAT C F NUMBER OF TEETH K ACCESSORY THREAD E MATING THREAD J THREAD 4 MINOR KEYWAYS "O" RING SEAL HEX NUT PER D38999/28 PANEL THICKNESS 3.20(.126) 1.58(.062) Page 38 Page 44 Pages 17-19 Page 37 Pages 15, 16 Page 42 Note 1: "K" Accessory Thread for AE324 is same as AE326 ("D" Accessory Thread) on page 41. Completed Part Number Contacts, Sealing Plugs and Tools Insert Arrangements Performance Specifications Insert Availability and Contact Information Polarization Note 2: "E" Mating Thread for AE324 is same as AE326 ("E" Mating Thread) on page 41 except it is Class 2A. Note 3: Maximum Grommet Extension for insert layouts incorporating size 8 and 10 contacts = 5.95(.234). A B C D +.10 -.15 +.60 -.00 +.90 -.10 J Maximum Jam Nut Thread inch mm inch mm inch mm inch mm inch mm inch mm 0.100R 1.063 27.00 .651 16.53 .945/.859 24.00/21.82 .555 14.10 12 .087 2.20 .299 7.59 M17x1-6g 1.252 31.80 .751 19.07 1.063/.984 27.00/24.99 .555 14.10 16 .087 2.20 .427 10.85 M20x1-6g A B +.035 -.004 H +.004 -.006 .016 No. of Teeth G .40 Shell Size +.024 -.000 F C 1.374 34.90 .938 23.82 1.260/1.172 32.00/29.77 .555 14.10 20 .087 2.20 .541 13.74 M25x1-6g D 1.500 38.10 1.062 26.97 1.417/1.296 36.00/32.91 .555 14.10 24 .087 2.20 .666 16.92 M28x1-6g E 1.626 41.30 1.187 30.15 1.457/1.422 37.00/36.12 .555 14.10 28 .087 2.20 .791 20.09 M32x1-6g F 1.811 46.00 1.312 33.32 1.614/1.546 41.00/39.26 .555 14.10 32 .118 3.00 .897 22.78 M35x1-6g G 1.937 49.20 1.437 36.50 1.811/1.672 46.00/42.47 .555 14.10 36 .118 3.00 1.022 25.96 M38x1-6g H 2.063 52.40 1.562 39.67 1.969/1.796 50.00/45.61 .555 14.10 40 .118 3.00 1.147 29.13 M41x1-6g J 2.189 55.60 1.687 42.85 2.017/1.939 51.23/49.25 .555 14.10 44 .118 3.00 1.272 32.31 M44x1-6g www.conesys.com - 40 - sales@aero-electric.com D38999/26 Self-Locking, RFI Grounding Plug AE326 Triple Start Threaded Coupling, Crimp Removable, Rear Release, Scoop-Proof 31.00(1.220) MAX [ A BLUE COLOR BAND LOCATION OPTIONAL (REAR RELEASE) MASTER KEY MAX COUPLING NUT 2.16(.085) MAX GROMMET EXTENSION 7.11(.280) MIN FULL THREAD [ B RFI STRIP MIL-DTL- 38999 S III MAX GROMMET T NUMBER OF TEETH E MATING THREAD 4 MINOR KEYS Page 38 Page 44 Pages 17-19 Page 37 Pages 15, 16 Page 42 D ACCESSORY THREAD Completed Part Number Contacts, Sealing Plugs and Tools Insert Arrangements Performance Specifications Insert Availability and Contact Information Polarization Note : Maximum Grommet Extension for insert layouts incorporating size 8 and 10 contacts = 5.95(.234). A B D E T Maximum Maximum Accessory Thread Metric Mating Thread Class 2B No. of Teeth Shell Size inch mm inch mm A .858 21.80 .299 7.59 M12x1.0-6g 0.100R .6250-0.1P-0.3L 12 B .984 25.00 .427 10.85 M15x1.0-6g 0.100R .7500-0.1P-0.3L 16 C 1.157 29.40 .541 13.74 M18x1.0-6g 0.100R .8750-0.1P-0.3L 20 D 1.280 32.50 .666 16.92 M22x1.0-6g 0.100R 1.0000-0.1P-0.3L 24 E 1.406 35.70 .791 20.09 M25x1.0-6g 0.100R 1.1875-0.1P-0.3L 28 F 1.516 38.50 .897 22.78 M28x1.0-6g 0.100R 1.2500-0.1P-0.3L 32 G 1.642 41.70 1.022 25.96 M31x1.0-6g 0.100R 1.3750-0.1P-0.3L 36 H 1.768 44.90 1.147 29.13 M34x1.0-6g 0.100R 1.5000-0.1P-0.3L 40 J 1.890 48.00 1.272 32.31 M37x1.0-6g 0.100R 1.6250-0.1P-0.3L 44 www.conesys.com - 41 - sales@aero-electric.com MIL-DTL-38999 Polarization Series III Keying Positions D NORMAL MASTER KEYWAY A B C MIL-DTL- 38999 S III Notes: 1. Mating face of receptacle shown (plug is opposite). 2. All minor keyways (keys) are rotated to provide shell polarization while master keyway (key) remains fixed as shown. 3. The angles for a given connector are the same whether it contains pin or socket inserts. 4. Insert arrangement does not rotate relative to the master keyway (key). Key/Keyway Shell Size Key/Keyway Positions BSC Identification Letter N A B C D E A 105 102 80 35 64 91 B 140 132 118 140 155 131 C 215 248 230 205 234 197 D 265 320 312 275 304 240 B (11) C (13) D (15) N A B C D E 95 113 90 53 119 51 141 156 145 156 146 141 208 182 195 220 176 184 236 292 252 255 298 242 E (17) F (19) G (21) H (23) J (25) N A B C D E 80 135 49 66 62 79 142 170 169 140 145 153 196 200 200 200 180 197 293 310 244 257 280 272 A (9) www.conesys.com - 42 - sales@aero-electric.com MIL-DTL-38999 Series III Flange and Jam Nut Receptacles Panel Cutouts Panel Cutouts JAM NUT FLANGE MOUNT 3.20(.126) 1.58(.062) PANEL THICKNESS 4x [ C [B MIN MIL-DTL- 38999 S III D [E A Note: Diameter B cutout dimensions are listed separately for back and front of panel mounting. A B B C (TP) For Back Mounting Minimum For Front Mounting Minimum D +.00 -.25 +.010 -.000 inch mm inch mm .670 17.02 .700 17.78 .771 19.59 .825 20.96 .13 +.000 -.010 inch mm .128 3.25 15.88 .128 3.25 Shell Size inch mm inch mm inch mm A (9) .719 18.26 .656 16.66 .516 13.11 B (11) .812 20.62 .796 20.22 .625 .005 E +.25 -.00 C (13) .906 23.01 .922 23.42 .750 19.05 .128 3.25 .955 24.26 1.010 25.65 D (15) .969 24.61 1.047 26.59 .906 23.01 .128 3.25 1.085 27.56 1.135 28.83 E (17) 1.062 26.97 1.219 30.96 1.016 25.81 .128 3.25 1.210 30.73 1.260 32.01 F (19) 1.156 29.36 1.297 32.94 1.141 28.98 .128 3.25 1.335 33.91 1.385 35.18 G (21) 1.250 31.75 1.422 36.12 1.266 32.16 .128 3.25 1.460 37.08 1.510 38.35 H (23) 1.375 34.93 1.547 39.29 1.375 34.93 .154 3.91 1.585 40.26 1.635 41.53 J (25) 1.500 38.10 1.672 42.47 1.484 37.69 .154 3.91 1.710 43.43 1.760 44.70 www.conesys.com - 43 - sales@aero-electric.com MIL-DTL-38999 Contacts, Tools and Seal Plugs Series III Contacts, Plastic Insertion/Removal Tools and Seal Plugs Contact Size MIL-DTL- 38999 S III 22D 20 16 12 12 Coax 12 Coax 10 (Power) 8 Coax 8 Twinax Application Pin Contacts Socket Contacts Seal Plugs Insertion/Removal Tools Type Power/Signal Power/Signal Power/Signal Power/Signal Coax Coax Power Coax Twinax Military No. M39029/58-360 M39029/58-363 M39029/58-364 M39029/58-365 M39029/28-211 M39029/102-558 M39029/58-528 M39029/60-367 M39029/90-529 Military No. M39029/56-348 M39029/56-351 M39029/56-352 M39029/56-353 M39029/75-416 M39029/103-559 M39029/56-527 M39029/59-366 M39029/91-530 Military No. MS27488-22-1 MS27488-20 -1 MS27488-16 -1 Plastic Military No. M81969/14-01 M81969/14-10 M81969/14-03 MS27488-12-1 M81969/14-04 M85049/81-10*** MS27488-8-1 MS27488-8-1 M81969/14-05 M81969/14- 06 M81969/14-12 Positioner Positioner Insertion Tool Extraction Tool For Socket Contacts Military No. M22520/2-07 M22520/1-04 M22520/2-10 M22520/1-04 M22520/1-04 M22520/2-34 M22520/31-02 N/A M22520/2-31 M22520/5-05 Die Closure B M22520/2-37 Metal Military No. M81969/8-01 Metal Military No. M81969/8-02 M81969/8-05 M81969/8-06 M81969/8-07 M81969/8-08 M81969/8-09 M81969/8-10 M81969/8-11 M81969/8-12 M81969/8-13** M81969/8-14 M22520/5-200 -- -- Crimping and Metal Insertion/Extraction Tools Crimp Tool 16 12 12 Coax Inner 12 Coax Outer 10 ( Power) 8 Coax Inner Military No. M22520/2- 01 M22520/1- 01 M22520/2-01 M22520/1-01 M22520/1-01 M22520/2-01 M22520/31-01 1716P-1**** M22520/2-01 8 Coax Outer M22520/5-01 8 Twinax Center M22520/2-01 For Pin Contacts Military No. M22520/2-09 M22520/1-04 M22520/2-10 M22520/1-04 M22520/1-04 M22520/2-34 M22520/31-02 N/A M22520/2-31 M22520/5-05 Die Closure B M22520/2-37 8 Twinax Outer & Intermediate M22520/5-01 M22520/5-200 Contact Size/Type 22D 20 Contact and Wire Data Contact Size 22D 20 16 12 10 Test Current* Voltage* DC Test Amps 5.0 7.5 13.0 23.0 33.0 Max. Drop Millivolts 73 55 49 42 33 Crimp Well Data Well Dia. inch .0345 .0010 .047 .001 .067 .001 .100 .002 .137 .003 Minimum Well Dept inch mm .141 3.58 .209 5.31 .209 5.31 .209 5.31 .355 9.02 AWG 28-22 24-20 20-16 14-12 12-10 mm2 .08-.33 .20-.52 .52-1.31 2.08-3.31 3.31-5.26 Finished Wire Range Minimum inch mm .030 .76 .040 1.02 .065 1.65 .097 2.46 .135 3.42 Maximum inch mm .054 1.37 .083 2.11 .109 2.77 .142 3.61 .162 4.12 Note: Size 8 coax contacts are used with M17/095-RG180 cable, while size 8 Twinax contacts are used with M17/176-00002 cable. MS3348 bushing required with 12 gauge wire. * When tested with silver-plated wire. ** Insertion tool is not required. *** Dummy contact, used in lieu of unwired contact and seal plug. **** Daniels Manufacturing part number. www.conesys.com Wire Range - 44 - sales@aero-electric.com MIL-DTL-38999 Contact Installation Instructions Series III Contact Installation Instructions 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. Crimping Contacts 1. Select the appropriate crimp tool and ensure that the proper crimp head positioner is used. 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. 2. Cycle the tool to be sure the indentors are open. 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. 4. Place the contact, mating end first, into the tool. 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. 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. Completion After all the cavities have been filled, slide the hardware back into position on the connector and tighten. 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. 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. 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. Size Pin Contact Socket Contact Basic Crimp Tool Pin Positioner Socket Positioner Insertion/Removal Tool 22D M39029/58-360 M39029/56-348 M22520/2-01 M22520/1-01 M22520/2-09 M22520/07 M81969/14-01 M22520/1-04 Red M22520/1-04 red M22520/2-01 M22520/2-10 M22520/2-10 20 M39029/58-363 M39029/56-351 16 M39029/58-364 M39029/56-352 M22520/1-01 M22520/1-04 Blue M22520/1-04 Blue M81969/14-03 12 M39029/58-365 M39029/56-353 M22520/1-01 M22520/1-04 Yellow M22520/1-04 Yellow M81969/14-04 10 M39029/58-528 M39029/56-527 * * * M81969/14-05 For Coax and Twinax contacts refer to instructions that are supplied with contacts. www.conesys.com M81969/14-10 * Contact Daniels Manufacturing for crimp tool/positioner. - 45 - sales@aero-electric.com MIL-DTL- 38999 S III 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.