from the desk of james plessas 1 of 1 6.0/10.0 detail-a - - sym. description date approved revisions GAP-027 2 preliminary 04/18/06 tmh 319 series swing arm clamp shield sock termination procedure 2 approved 05-5368 gap GAP-027 03/16/05 03/16/05 03/16/05 j. plessas j. plessas k. bailey - + release date non repairable commercial item cad 1991 n/a n/a 1 of 3 c 1211 air way - glendale - california 91201 2 + .015 .xxx .03 .xx - + 1/16 + angles decimals fractions tolerances: dimensions are in inches unless otherwise specified do not scale this drawing b/f p/c engr check drawn 06324 approved release date original size code ident. no. scale weight sheet rev. d 2.00 min tap wrap under ring to ensure snug fit jacket (if applicable) overall braid from wire bundle (if applicable) overall braid from backshell conductor straight configuration 45 configuration 90 configuration figure 1 4. insert wire bundle into adapter and bottom against the connector. hold cable and mark or tag location where shield support ring, glenair p/n 687-207, will be located. this distance may vary upon accepted technique of user and flexibility of bundle immediately rear of saddles. (figure 1) 5. at the marked location, where the shield support ring is located, wrap tape around wire bundle for snug fit of shield support ring.(figure 1) (optional tape wrap) 6. slide overall braid from wire bundle side over shield support ring. trim braid ends and tuck extra length braid underneath itself, creating a clean appearance. (skip step if wire bundle does not have a overall braid) 7. pin connector, slide backshell forward, and hand tighten backshell to connector. steps: the following suggested procedure is a guide for proper assembly and installation of glenair's 319 series swing arm braid sock adapters. it is recommended that trial samples of appropriate shield wire bundles be used to determine proper trim dimensions of the cable jacket (if applicable), individual shields and conductors. 1. assemble swing arm clamp to desired configuration tightening screws to lock arms in place (straight, 45, or 90 configuration) leaving saddle clamp hardware loose. 2. insert wire bundle into backshell to determine if braid transition angle from backshell to wire bundle is less than 45. if the transition is less that 45 build up wire bundle with tape and re-insert wire bundle into backshell as shown (figure 1a) to support the transition of overall braid from backshell to the wire bundle 3. temporarily assemble adapter to connector (not shown) and push back backshell braid. figure 1a wire bundle optional tape wrap braid transition angle 2 687-207 split shield support ring optional tape wrap 5 2 caution: loosen saddle clamps to allow free cable movement before adjusting clamp to angular positions. form the cable into the desired configuration, then tighten arms and secure the saddle clamps. .38 window strip 1.5/3.0 (optional) contact wire shrink sleeve exposed braid solder sleeve pigtail tying cord tsp jacket detail-a 1.7/3.7 14
from the desk of james plessas 1 of 1 2 steps: cont'd 8. evenly space shield pigtails (figure 2) or solder sleeve pigtails (figure 3) around shield support ring. cut pigtails so that end of pigtails are approximately .50 beyond end of shield support ring. 9. bring shield sock from backshell and completely cover pigtails and support ring. trim and fold braid as shown in figure 4. lace tie shield adjacent to support ring ends. 10. install band, 600-052, per glenair's band-it termination process between the lace ties onto the center of the support ring, as shown (figure 4). hand banding tool, 600-058, or pneumatic banding tool, 600-067, required for banding process. 11. wrap shield support ring assembly with high temperature tape, using 50% overlap (not shown). d rev. sheet weight scale code ident. no. size original release date approved 06324 drawn check engr p/c b/f do not scale this drawing unless otherwise specified dimensions are in inches tolerances: fractions decimals angles + 1/16 + - .xx .03 .xxx .015 + 2 1211 air way - glendale - california 91201 c 2 of 3 n/a n/a cad 1991 non repairable commercial item release date + - k. bailey j. plessas j. plessas 03/16/05 03/16/05 03/16/05 GAP-027 gap 05-5368 approved 2 319 series swing arm clamp shield sock termination procedure see sheet 1 GAP-027 revisions approved date description sym. - - 600-052 lacing string or high temperature ty-strap 1.00 approx. lacing string or high temperature ty-strap 1.00 max .50 approx. figure 2 figure 4 figure 3 support ring tuck braid as shown conductors shield pigtail equally space pigtails around ring stagger solder sleeves lacing string or high temperature ty-strap
from the desk of james plessas 1 of 1 arm screw installation torque (in lb) 4 4 6 6 6 6 6 6 6 - - - 14 arm screw size 4 4 6 6 6 6 6 6 6 - - - saddle screw size 4 4 6 6 6 6 6 6 6 6 10 10 saddle screw arm screw 14 13 13 1.00 approx. 102-080 expando sleeve braid sock lacing string or high temperature ty-straps applied in 1.00 inch increments optional (lacing must be placed over window strip area) figure 5 - - sym. description date approved revisions GAP-027 see sheet 1 319 series swing arm clamp shield sock termination procedure 2 approved 05-5368 gap GAP-027 03/16/05 03/16/05 03/16/05 j. plessas j. plessas k. bailey - + release date non repairable commercial item cad 1991 n/a n/a 3 of 3 c 1211 air way - glendale - california 91201 2 + .015 .xxx .03 .xx - + 1/16 + angles decimals fractions tolerances: dimensions are in inches unless otherwise specified do not scale this drawing b/f p/c engr check drawn 06324 approved release date original size code ident. no. scale weight sheet rev. d lace tie, tape, or shrink sleeve may be used to dress ends steps: cont'd 12. place lacing cord, high temperature tape, or high temperature plastic ty-straps in 1.00 increments starting at the braid transition rear of the backshell to secure over braid on wire bundle. cover over braid with 102-080 braid sock extending approximately 1.00 inches past shield support ring. (figure 5) optional 13. securely tighten adapter to connector using glenair 600-091 composite hex coupling torque wrench and other tooling accessories to established torque values. (see table i) 14. secure the strain relief saddle onto the wire bundle using tg69 soft jaw pliers to firmly hold saddles down evenly onto wire bundle. torque screws to values shown in table i. suggest using teflon tape wrap or m85049/127 bushing strip, as needed, to cusion braid sock under the saddle clamps. 15. see glenair drawing 687-654, 687-655 & 687-656 for saddle bar replacement parts. coupling ring installation torque (in lb) table i connector shell size ref 08,09,a 10,11,b 12,13,c 14,15,d 16,17,e 18,19,f 20,21,g 22,23,h 24,25,j 28 32 36 35 40 40 40 40 40 80 80 80 120 120 120 4 4 6 6 6 6 6 6 6 6 10 10 hex coupling torque wrench 600-091-08 600-091-10 600-091-12 600-091-14 600-091-16 600-091-18 600-091-20 600-091-22 600-091-24 600-091-28 600-091-32 600-091-36 saddle screw installation torque (in lb) 2
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