INCH-POUND MS3114M 15 January 2015 SUPERSEDING MS3114L 4 June 2009 DETAIL SPECIFICATION SHEET CONNECTORS, RECEPTACLE, ELECTRICAL, SERIES 1, SOLDER TYPE, JAM NUT MOUNTING, BAYONET COUPLING, CLASSES E, F, H AND P Inactive for new design after 10 June 1993. For new design, use MS3474 for classes E, F, and P. This specification is approved for use by all Departments and Agencies of the Department of Defense. The requirements for acquiring the product described herein shall consist of this specification sheet and MIL-DTL-26482. STYLE P, PIN INSERT FIGURE 1. Dimensions and configurations for classes E, F and P. AMSC N/A FSC 5935 Source: https://assist.dla.mil -- Downloaded: 2015-05-19T07:58Z Check the source to verify that this is the current version before use. MS3114M STYLE S, SOCKET INSERT FIGURE 1. Dimensions and configurations for classes E, F and P - Continued. 2 Source: https://assist.dla.mil -- Downloaded: 2015-05-19T07:58Z Check the source to verify that this is the current version before use. MS3114M A max length B dia +.000 -.032 across flange corner C +.000 -.010 mtg flat 8 .954 (24.23) 1.078 (27.38) .530 (13.46) .540 (13.72) 10 1.078 (27.38) 1.203 (30.56) .655 (16.64) .665 (16.89) 12 1.266 (32.16) 1.391 (35.33) .818 (20.78) .828 (21.03) 14 1.391 (35.33) 1.516 (38.51) .942 (23.93) .952 (24.18) 16 1.516 (38.51) 1.641 (41.68) 1.066 (27.08) 18 1.641 (41.68) 1.766 (44.86) 20 1.828 (46.43) 22 24 Shell size E F +.010 min mounting -.005 panel flat thread location location G .020 thick mtg flange K + .010 J - .005 O-ring panel seal SAE-AS29513- mounting hole 017 .572 (14.53) 019 .697 (17.70) 022 .885 (22.48) 024 1.010 (25.65) 1.076 (27.33) 026 1.135 (28.83) 1.191 (30.25) 1.201 (30.51) 028 1.260 (32.00) 1.954 (49.63) 1.316 (33.43) 1.326 (33.68) 128 1.385 (35.18) 1.954 (49.63) 2.078 (52.78) 1.441 (36.60) 1.451 (36.86) 130 1.510 (38.35) 2.078 (52.78) 2.203 (55.96) 1.566 (39.78) 1.576 (40.03) 132 1.635 (41.53) .117 (2.97) .384 (9.75) .446 (11.33) .148 (3.76) .479 (12.17) FIGURE 1. Dimensions and configurations for classes E, F and P - Continued. 3 Source: https://assist.dla.mil -- Downloaded: 2015-05-19T07:58Z Check the source to verify that this is the current version before use. MS3114M Shell size M + .031 - .000 mounting flange location N UNEF-2B accessory thread R max ID gasket S panel thick ref min T .011 O-ring projection V UNEF-2A mounting thread max 8 .625-24 .329 (8.36) .5625-24 10 .750-20 .457 (11.61) .6875-24 12 .875-20 .564 (14.33) 1.000-20 .689 (17.50) 16 1.125-18 .814 (20.68) 18 1.250-18 .907 (23.04) 1.250-18 1.375-18 1.039 (26.39) 1.375-18 1.500-18 1.164 (29.57) 1.625-18 1.289 (32.74) 14 .691 (17.55) 20 22 24 .879 (22.33) .912 (23.16) .125 (3.18) .023 (0.58) .062 (1.57) .875-20 1.000-20 1.125-18 .250 (6.35) .028 (0.71) 1.500-18 1.625-18 FIGURE 1. Dimensions and configurations for classes E, F and P - Continued. 4 Source: https://assist.dla.mil -- Downloaded: 2015-05-19T07:58Z Check the source to verify that this is the current version before use. MS3114M CLASS E DIMENSIONS FOR CLASS E Shell size 8 10 12 14 16 18 20 22 24 L max overall length 1.344 (34.14) 1.594 (40.49) 1.641 (41.68) X dia min ID .269 (6.83) .359 (9.12) .469 (11.91) .589 (14.96) .717 (18.21) .779 (19.79) .901 (22.89) 1.009 (25.63) 1.123 (28.52) Y dia max OD .750 (19.05) .875 (22.23) 1.000 (25.40) 1.125 (28.58) 1.250 (31.75) 1.375 (34.93) 1.531 (38.89) 1.656 (42.06) 1.781 (45.24) FIGURE 1. Dimensions and configurations for classes E, F and P - Continued. 5 Source: https://assist.dla.mil -- Downloaded: 2015-05-19T07:58Z Check the source to verify that this is the current version before use. MS3114M CLASS F DIMENSIONS WITH BUSHING, CLASS F DIMENSIONS WITH BUSHING REMOVED, CLASS F FIGURE 1. Dimensions and configurations for classes E, F and P - Continued. 6 Source: https://assist.dla.mil -- Downloaded: 2015-05-19T07:58Z Check the source to verify that this is the current version before use. MS3114M DIMENSIONS FOR CLASS F Shell size L max overall length 8 10 12 1.906 (48.41) 14 16 2.047 (51.99) 18 2.078 (52.78) 20 22 24 2.328 (59.13) 2.453 (62.31) X dia min open Y max .234 (5.94) .297 (7.54) .422 (10.72) .828 (21.03) .547 (13.89) 1.141 (28.98) .609 (15.47) 1.203 (30.56) .734 (18.64) 1.469 (37.31) .922 (23.42) 1.656 (42.06) .984 (24.99) 1.750 (44.45) .891 (22.63) 1.016 (25.81) V max closed N free dia .187 (4.75) .187 (4.75) .281 (7.14) .325 (8.26) .356 (9.04) .456 (11.58) .125 (3.18) .188 (4.78) .312 (7.92) .375 (9.53) .500 (12.70) .625 (15.88) .625 (15.88) .750 (19.05) .800 (20.32) .519 (13.18) .657 (16.69) .010 (see note 4) ZZ screw threads YZ Lockwashers NASM35338 or NASM35333 types (see note 5) 6-32 UNC NASM35338 -98 or -41 NASM35333 -105, -36 or -37 8-32 UNC NASM35338 -99 or -42 NASM35333 -106 or -38 FIGURE 1. Dimensions and configurations for classes E, F and P - Continued. 7 Source: https://assist.dla.mil -- Downloaded: 2015-05-19T07:58Z Check the source to verify that this is the current version before use. MS3114M CLASS P DIMENSIONS FOR CLASS P Shell size L max overall length 8 10 12 14 1.391 (35.33) 16 18 20 22 24 1.641 (41.68) 1.703 (43.26) X dia min ID .317 (8.05) .434 (11.02) .548 (13.92) .673 (17.09) .798 (20.27) .899 (22.83) 1.024 (26.01) 1.149 (29.18) 1.274 (32.36) Y dia max OD .608 (15.44) .734 (18.64) .858 (21.79) .984 (24.99) 1.110 (28.19) 1.234 (31.34) 1.360 (34.54) 1.484 (37.69) 1.610 (40.89) PP min .250 (6.35) FIGURE 1. Dimensions and configurations for classes E, F and P - Continued. 8 Source: https://assist.dla.mil -- Downloaded: 2015-05-19T07:58Z Check the source to verify that this is the current version before use. MS3114M Inches .005 .010 .011 .015 .016 .020 .023 .028 .031 .032 .062 .070 .117 .125 .148 .156 .187 .188 .234 .250 .259 .281 .297 .312 .317 .325 .329 .356 .359 mm 0.13 0.25 0.28 0.38 0.41 0.51 0.58 0.71 0.79 0.81 1.57 1.78 2.97 3.18 3.75 3.96 4.75 4.78 5.94 6.35 6.58 7.14 7.54 7.92 8.05 8.26 8.36 9.04 9.12 Inches .375 .384 .422 .430 .434 .446 .456 .457 .469 .479 .500 .519 .530 .540 .547 .548 .5625 .564 .572 .589 .608 .609 .625 .655 .657 .665 .673 .6875 .689 mm 9.52 9.75 10.72 10.92 11.02 11.33 11.58 11.61 11.91 12.17 12.70 13.18 13.46 13.72 13.89 13.92 14.288 14.33 14.53 14.96 15.44 15.47 15.88 16.64 16.69 16.89 17.09 17.462 17.50 Inches .691 .697 .717 .734 .750 .779 .798 .800 .814 .818 .828 .858 .875 .879 .885 .891 .899 .901 .907 .912 .922 .942 .952 .954 .984 1.000 1.009 1.010 1.016 mm 17.55 17.70 18.21 18.64 19.05 19.79 20.27 20.32 20.68 20.78 21.03 21.79 22.22 22.33 22.48 22.63 22.83 22.89 23.04 23.16 23.42 23.93 24.18 24.23 24.99 25.40 25.63 25.65 25.81 Inches 1.024 1.039 1.066 1.076 1.078 1.110 1.123 1.125 1.135 1.141 1.149 1.164 1.191 1.201 1.203 1.234 1.250 1.260 1.266 1.275 1.289 1.316 1.326 1.344 1.360 1.375 1.385 1.391 1.441 mm 26.01 26.39 27.08 27.33 27.38 28.19 28.52 28.58 28.83 28.98 29.18 29.59 30.25 30.51 30.56 31.34 31.75 32.00 32.16 32.39 32.74 33.43 33.68 34.14 34.54 34.92 35.18 35.33 36.60 Inches 1.451 1.469 1.484 1.500 1.510 1.516 1.531 1.566 1.576 1.549 1.610 1.625 1.635 1.641 1.656 1.703 1.750 1.766 1.781 1.828 1.906 1.954 2.047 2.078 2.203 2.328 2.453 NOTES: 1. 2. 3. 4. 5. 6. 7. Dimensions are in inches. Metric equivalents are given for information only. Intermateability dimensions shall be in accordance with MIL-DTL-26482. Use SAE-AS85049/139 bushing if reduced opening is required. Lock washers may be captive. Not for Air Force use. Use MS3474 in lieu of MS3114 classes E, F and P. True position (TP) tolerances specified are in accordance with ASME Y14.5. FIGURE 1. Dimensions and configurations for classes E, F and P - Continued. 9 Source: https://assist.dla.mil -- Downloaded: 2015-05-19T07:58Z Check the source to verify that this is the current version before use. mm 36.86 37.31 37.69 38.10 38.35 38.51 38.89 39.78 40.03 40.49 40.89 41.28 41.53 41.68 42.06 43.26 44.45 44.86 45.24 46.43 48.41 49.63 51.99 52.78 55.96 59.13 62.31 MS3114M STYLE P PIN INSERT FIGURE 2. Dimensions and configurations for class H. 10 Source: https://assist.dla.mil -- Downloaded: 2015-05-19T07:58Z Check the source to verify that this is the current version before use. MS3114M STYLE S SOCKET INSERT FIGURE 2. Dimensions and configurations for class H - Continued. 11 Source: https://assist.dla.mil -- Downloaded: 2015-05-19T07:58Z Check the source to verify that this is the current version before use. MS3114M A max length B dia + .000 - .032 across flange corner C + .000 - .010 mounting flat E + .010 - .005 panel mounting hole 8 .954 (24.23) 1.078 (27.38) .530 (13.46) .540 (13.72) 017 .572 (14.53) 10 1.078 (27.38) 1.203 (30.56) .655 (16.64) .665 (16.89) 019 .697 (17.70) 12 1.266 (32.16) 1.391 (35.33) .818 (20.78) .828 (21.03) 022 .885 (22.48) 14 1.391 (35.33) 1.516 (38.51) .942 (23.93) .952 (24.18) 024 1.010 (25.65) 16 1.516 (38.51) 1.641 (41.68) 1.066 (27.08) 1.076 (27.33) 026 1.135 (28.83) 18 1.641 (41.68) 1.766 (44.86) 1.191 (30.25) 1.201 (30.51) 028 1.260 (32.00) 20 1.828 (46.43) 1.954 (49.63) 1.316 (33.43) 1.326 (33.68) 128 1.385 (35.18) 22 1.954 (49.63) 2.078 (52.78) 1.441 (36.60) 1.451 (36.86) 130 1.510 (38.35) 24 2.078 (52.78) 2.203 (55.96) 1.566 (39.78) 1.576 (40.03) 132 1.635 (41.53) Shell size F min mounting thread location .384 (9.75) .446 (11.33) G .020 thick mounting flange J O-ring seal SAEAS29513- .117 (2.97) .148 (3.76) .479 (12.17) FIGURE 2. Dimensions and configuration for class H - Continued. 12 Source: https://assist.dla.mil -- Downloaded: 2015-05-19T07:58Z Check the source to verify that this is the current version before use. K + .010 - .005 panel mounting hole MS3114M Shell size L max M +.031 .000 mounting flange location 8 10 12 14 .875 (22.23) .691 (17.55) 16 18 20 22 24 1.094 (27.79) .879 (22.33) 1.125 (28.58) .912 (23.16) S panel thickness ref R max ID gasket Min .329 (8.36) .457 (11.61) .564 (14.33) .689 (17.50) .814 (20.68) .907 (23.04) 1.039 (26.39) 1.164 (29.57) 1.289 (32.74) T .011 O-ring projection V UNEF-2A mounting thread Max .5625-24 .6875-24 .875-20 .125 (3.18) .023 (.58) .062 (1.57) 1.000-20 1.125-18 1.250-18 1.375-18 .250 (6.35) .028 (.71) 1.500-18 1.625-18 Material and finish: a. Shell types A and B - passivated stainless steel shells with gold plated contacts. b. Shell types C and Y - tin-plated ferrous alloy shells with gold plated contacts (tin plating shall be no more than 97% pure tin and a minimum of 3% lead by mass). c. Bayonet pins - passivated stainless steel. FIGURE 2. Dimensions and configuration for class H - Continued. 13 Source: https://assist.dla.mil -- Downloaded: 2015-05-19T07:58Z Check the source to verify that this is the current version before use. MS3114M Inches .005 .010 .011 .015 .016 .020 .023 .028 .031 .032 .033 .062 .070 .117 .125 .148 .156 mm 0.13 0.25 0.28 0.38 0.41 0.51 0.58 0.71 0.79 0.81 0.84 1.57 1.78 2.97 3.18 3.75 3.96 Inches .250 .329 .384 .446 .457 .479 .530 .540 .5625 .564 .572 .655 .665 .6875 .689 .691 .697 mm 6.35 8.36 9.75 11.33 11.61 12.17 13.46 13.72 14.288 14.33 14.53 16.64 16.89 17.462 17.50 17.55 17.70 Inches .814 .818 .828 .875 .879 .885 .907 .912 .942 .952 .954 1.000 1.010 1.024 1.039 1.066 1.076 mm 20.68 20.78 21.03 22.22 22.33 22.48 23.04 23.16 23.93 24.18 24.23 25.40 25.65 26.01 26.39 27.08 27.33 Inches 1.078 1.094 1.125 1.135 1.164 1.191 1.201 1.203 1.250 1.260 1.266 1.289 1.316 1.326 1.375 1.385 1.391 mm 27.38 27.79 28.58 28.83 29.59 30.25 30.51 30.56 31.75 32.00 32.16 32.74 33.43 33.68 34.92 35.18 35.33 Inches 1.441 1.451 1.500 1.510 1.516 1.566 1.576 1.625 1.635 1.641 1.766 1.828 1.954 2.078 2.203 mm 36.60 36.69 38.10 38.35 38.51 39.78 40.03 41.28 41.53 41.68 44.86 46.43 49.63 52.78 55.96 NOTES: 1. Dimensions are in inches. 2. Metric equivalents are given for information only. 3. Intermateability dimensions shall be in accordance with MIL-DTL-26482. 4. Sealing member bonded to vitreous insert. 5. Not for Air Force use. Use MS3449 in lieu of MS3114 class H. 6. True position (TP) tolerances specified are in accordance with ASME Y14.5. 7. MS3114 class H is inactive for new design. For new design, use MS3449. FIGURE 2. Dimensions and configurations for class H - Continued. REQUIREMENTS: Dimensions and configuration: See figures 1 and 2. Connector mating: This connector mates with MS3116. For insert arrangement: See MIL-STD-1669. Sealing member (class H only): Bonded to vitreous insert. Packing material shall meet the requirements of ASTM-D2000. Finishes (classes E, F and P only): A finish designator shall not be included in the PIN when finish W is required. See MIL-DTL-26482 for alternative finish designators D, T and K for classes E, F and P. Material and finish (class H only): See figure 2. APPLICATION NOTE: MS3114 is similar to MS3474, except for the following: MS3474 utilizes crimp type rear release contacts, whereas connectors produced to this document utilize non-removable contacts with solderable terminations. Also, MS3474 does not include a hermetically sealed configuration. MS3114, class H, is similar to MS3449, series 2, class H, which has solder type terminations, and is also similar to MS3479, series 2, class N, which has crimp type terminations. 14 Source: https://assist.dla.mil -- Downloaded: 2015-05-19T07:58Z Check the source to verify that this is the current version before use. MS3114M Part or Identifying Number (PIN) examples: PIN example for classes E, F and P (see figure 1): MS3114 E 8 33 P W D MS number Class Shell size Insert arrangement Contact style Alternate insert position Finish Note: No finish designator is used when finish W is required (finish W is the default finish). PIN example for class H (see figure 2): MS3114 H 12 C 3 MS number Class Shell size Termination type, shell material, and shell and contact finish Insert arrangement Contact style Insert position 15 Source: https://assist.dla.mil -- Downloaded: 2015-05-19T07:58Z Check the source to verify that this is the current version before use. P W MS3114M Changes from previous issue. The margins of this specification sheet are marked with vertical lines to indicate where changes from the previous issue were made. This was done as a convenience only and the Government assumes no liability whatsoever for any inaccuracies in these notations. Bidders and contractors are cautioned to evaluate the requirements of this document based on the entire content irrespective of the marginal notations and relationship to the last previous issue. Referenced documents. In addition to MIL-DTL-26482, this document references the following: MIL-STD-1669 MS3116 MS3449 MS3474 MS3479 NASM35338 NASM35333 ASME Y14.5 ASTM-D2000 SAE-AS85049/139 CONCLUDING MATERIAL Custodians: Army - CR Navy - AS Air Force - 85 DLA - CC Preparing activity: DLA - CC (Project 5935-2015-033) Review activities: Army - AR, AV Navy - EC, SH Air Force - 99 NOTE: The activities listed above were interested in this document as of the date of this document. Since organizations and responsibilities can change, you should verify the currency of the information above using the ASSIST Online database at https://assist.dla.mil. 16 Source: https://assist.dla.mil -- Downloaded: 2015-05-19T07:58Z Check the source to verify that this is the current version before use.