319AS137XB10 Glenair

Composite Backshells 319-137 Composite Shield Sock Strain Relief with Self-Locking Rotatable Coupling Product Series Optional Braid Material CONNECTOR DESIGNATOR: 319 - EMI/RFI Shield B - See Table IV for Options Sock Assemblies (Omit for Std. Nickel/Copper) MIL-DTL-5015, -26482 Series II, A and -83723 Series I and III Angle and Profile A Custom Braid Length Finish Symbol S - Straight MIL-DTL-38999 Series I, II (see note 3) F Specify In Inches A - 90 (See Table III) (Omit for Std. 12 Length) B - 45 MIL-DTL-38999 Series III and IV H SELF-LOCKING 319 H S 137 XO 15 B R - 14 ROTATABLE COUPLING Connector Connector Designator Split Ring / Band Option Basic Part LOW PROFILE B Shell Size A, F, and H Number Split Ring (687-749) and Band (See Table II) (600-052-1) supplied with R option (Omit for none) Anti-Rotation Device L EMI Shroud Std. Shield IAW E C 107-030 Nickel/Copper Closed See Table III for Optional Material M F .25 Max 12.00 Min Screw Extension D Standard Length K H Crimp Ring Termination Area Free of Cadmium E G J Detail Finish XN .125 Dia. Drain Hole Screw Head Same 3 Min. Equally Spaced Side Typ Sym and Typ Sym and F Band (600-052-1) Split ring (687-749) G 2009 Glenair, Inc. Printed in U.S.A. CAGE Code 06324 GLENAIR, INC. 1211 AIR WAY GLENDALE, CA 91201-2497 818-247-6000 FAX 818-500-9912 www.glenair.com E-Mail: sales glenair.com A-22 Rev. 12 FEBRUARY 2013319-137 Composite Shield Sock Strain Relief with Self-Locking Rotatable Coupling TABLE II: SHELL SIZE Shell Size E F G H .031 Min Max Max A, F H 08 09 .265 (6.7) .22 (5.6) .901 (22.9) 1.388 (35.3) A 10 11 .310 (7.9) .27 (6.9) .964 (24.5) 1.428 (36.3) 12 13 .390 (9.9) .35 (8.9) 1.050 (26.7) 1.498 (38.0) 14 15 .506 (12.9) .47 (11.9) 1.112 (28.2) 1.548 (39.3) 16 17 .591 (15.0) .55 (14.0) 1.175 (29.8) 1.648 (41.9) 18 19 .661 (16.8) .62 (15.7) 1.230 (31.2) 1.768 (44.9) 20 21 .744 (18.9) .70 (17.8) 1.293 (32.8) 1.808 (45.9) B 22 23 .826 (21.0) .78 (19.8) 1.365 (34.7) 1.858 (47.2) 24 25 .896 (22.8) .85 (21.6) 1.417 (36.0) 1.898 (48.2) TABLE II: SHELL SIZE (CONTINUED) Shell Size K Diameter J K L Max Max Max A, F H A Code F Code H Code 08 09 .91 (23.1) 1.128 (28.7) .939 (23.9) .265 (6.7) .275 (7.0) .264 (6.7) C 10 11 .97 (24.6) 1.168 (29.7) 1.059 (26.9) .370 (9.4) .412 (10.5) .390 (9.9) 12 13 1.06 (26.9) 1.248 (31.7) 1.199 (30.5) .506 (12.9) .526 (13.4) .504 (12.8) 14 15 1.16 (29.5) 1.368 (34.7) 1.199 (30.5) .580 (14.7) .651 (16.5) .630 (16.0) 16 17 1.34 (34.0) 1.448 (36.8) 1.329 (33.8) .705 (17.9) .776 (19.7) .756 (19.2) 18 19 1.41 (35.8) 1.528 (38.8) 1.509 (38.3) .784 (19.9) .872 (22.1) .843 (21.4) 20 21 1.53 (38.9) 1.648 (41.9) 1.609 (40.9) .909 (23.1) 1.007 (25.6) .969 (24.6) D 22 23 1.66 (42.2) 1.688 (42.9) 1.759 (44.7) 1.034 (1.034) 1.132 (28.8) 1.091 (27.7) 24 25 1.78 (45.2) 1.758 (44.7) 1.859 (47.2) 1.149 (29.2) 1.257 (31.9) 1.217 (30.9) TABLE III: FINISH Symbol Finish Composite MaterialNo Plating, TABLE IV: BRAID TYPE XB Color Black, Brass Interface Shroud and AdapterNickel Plated Symbol Braid Type E A 100% AmberStrand 2000 Hour Corrosion Resistant B 75%/25% AmberStrand Blend XMT Ni-PTFE, Nickel-Fluorocarbon TM TM Polymer. 1000 Hour Grey L 100% ArmorLite Standard Nickel/Copper 34awg Composite MaterialNo Plating, T Tin/Copper 34awg Color Black and Brown, Brass XN Interface Shroud and Adapter Selectively Cadmium Plated F (See Detail B) NOTES 1. See composite thermoplastic shield sock assembly procedure for detailed installation instructions. 2. See Table I in Intro for front-end dimensional details. 3. Add mod code -475 to end of part number for use with Series II connectors. Backshell to be supplied less shroud. 4. Coupling nut supplied unplated. G 2009 Glenair, Inc. CAGE Code 06324 Printed in U.S.A. GLENAIR, INC. 1211 AIR WAY GLENDALE, CA 91201-2497 818-247-6000 FAX 818-500-9912 www.glenair.com E-Mail: sales glenair.com A-23 Rev. 12 FEBRUARY 2013 Composite Backshells