GAP-027

From the desk of James Plessas GAP-027 REVISIONS SYM. 2 DESCRIPTION PRELIMINARY DATE APPROVED 04/18/06 TMH 6.0/10.0 2.00 MIN TAP WRAP UNDER RING TO ENSURE SNUG FIT 1.7/3.7 JACKET (IF APPLICABLE) .38 WINDOW STRIP 1.5/3.0 (OPTIONAL) DETAIL-A CONDUCTOR PIGTAIL WIRE CONTACT OVERALL BRAID FROM BACKSHELL OPTIONAL TAPE WRAP 5 687-207 SPLIT SHIELD SUPPORT RING 2 BRAID TRANSITION ANGLE OVERALL BRAID FROM WIRE BUNDLE (IF APPLICABLE) TSP JACKET TYING CORD SOLDER SLEEVE EXPOSED BRAID SHRINK SLEEVE STRAIGHT CONFIGURATION DETAIL-A FIGURE 1 OPTIONAL TAPE WRAP 45° CONFIGURATION WIRE BUNDLE STEPS: FIGURE 1A 14 CAUTION: 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. 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. 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. 4. 90° CONFIGURATION UNLESS OTHERWISE SPECIFIED DIMENSIONS ARE IN INCHES TOLERANCES: FRACTIONS DECIMALS ANGLES APPROVED 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) CAD 1991 C 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) DRAWN K. BAILEY 03/16/05 CHECK J. PLESSAS 03/16/05 ENGR J. PLESSAS 03/16/05 1211 AIR WAY - GLENDALE - CALIFORNIA 91201 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) + - 1/16 +.03 .XX .XXX +.015 +2 DO NOT SCALE THIS DRAWING 2 319 SERIES SWING ARM CLAMP SHIELD SOCK TERMINATION PROCEDURE APPROVED RELEASE DATE ORIGINAL RELEASE DATE CODE IDENT. NO. SIZE 7. PIN CONNECTOR, SLIDE BACKSHELL FORWARD, AND HAND TIGHTEN BACKSHELL TO CONNECTOR. 06324 B/F 05-5368 P/C GAP NON REPAIRABLE COMMERCIAL ITEM SCALE N/A WEIGHT D GAP-027 N/A SHEET REV. 2 1 OF 3 1 of 1 From the desk of James Plessas GAP-027 REVISIONS SYM. DESCRIPTION SEE SHEET 1 DATE APPROVED LACING STRING OR HIGH TEMPERATURE TY-STRAP TUCK BRAID AS SHOWN SUPPORT RING STAGGER SOLDER SLEEVES FIGURE 3 1.00 APPROX. 600-052 CONDUCTORS .50 APPROX. 1.00 MAX SHIELD PIGTAIL LACING STRING OR HIGH TEMPERATURE TY-STRAP EQUALLY SPACE PIGTAILS AROUND RING FIGURE 2 LACING STRING OR HIGH TEMPERATURE TY-STRAP STEPS: CONT'D FIGURE 4 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. UNLESS OTHERWISE SPECIFIED DIMENSIONS ARE IN INCHES TOLERANCES: FRACTIONS DECIMALS ANGLES APPROVED 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. CAD 1991 C DRAWN K. BAILEY 03/16/05 CHECK J. PLESSAS 03/16/05 ENGR J. PLESSAS 03/16/05 1211 AIR WAY - GLENDALE - CALIFORNIA 91201 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). + - 1/16 +.03 .XX .XXX +.015 +2 DO NOT SCALE THIS DRAWING 2 319 SERIES SWING ARM CLAMP SHIELD SOCK TERMINATION PROCEDURE APPROVED RELEASE DATE ORIGINAL RELEASE DATE CODE IDENT. NO. SIZE 06324 B/F 05-5368 P/C GAP NON REPAIRABLE COMMERCIAL ITEM SCALE N/A WEIGHT D GAP-027 N/A SHEET REV. 2 2 OF 3 1 of 1 From the desk of James Plessas GAP-027 TABLE I SYM. DESCRIPTION SEE SHEET 1 DATE REVISIONS APPROVED SADDLE SCREW SIZE 4 4 6 6 6 6 6 6 6 6 10 10 4 4 6 6 6 6 6 6 6 6 10 10 4 4 6 6 6 6 6 6 6 4 4 6 6 6 6 6 6 6 SIZE CONNECTOR SHELL SIZE REF ARM SCREW COUPLING RING INSTALLATION TORQUE (IN LB) 13 HEX COUPLING TORQUE WRENCH 13 SADDLE SCREW INSTALLATION TORQUE (IN LB) 14 ARM SCREW INSTALLATION TORQUE (IN LB) 14 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 80 120 120 120 600-091-08 600-091-10 600-091-12 600-091-14 600-091-16 600-091-18 600-091-20 600-091-22 600-091-24 600-091-28 600-091-32 600-091-36 LACING STRING OR HIGH TEMPERATURE TY-STRAPS APPLIED IN 1.00 INCH INCREMENTS OPTIONAL (LACING MUST BE PLACED OVER WINDOW STRIP AREA) 1.00 APPROX. ARM SCREW SADDLE SCREW 102-080 EXPANDO SLEEVE BRAID SOCK LACE TIE, TAPE, OR SHRINK SLEEVE MAY BE USED TO DRESS ENDS FIGURE 5 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 C 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) UNLESS OTHERWISE SPECIFIED DIMENSIONS ARE IN INCHES TOLERANCES: FRACTIONS DECIMALS ANGLES CAD 1991 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. DRAWN K. BAILEY 03/16/05 CHECK J. PLESSAS 03/16/05 ENGR J. PLESSAS 03/16/05 1211 AIR WAY - GLENDALE - CALIFORNIA 91201 SUGGEST USING TEFLON TAPE WRAP OR M85049/127 BUSHING STRIP, AS NEEDED, TO CUSION BRAID SOCK UNDER THE SADDLE CLAMPS. APPROVED 15. SEE GLENAIR DRAWING 687-654, 687-655 & 687-656 FOR SADDLE BAR REPLACEMENT PARTS. + - 1/16 +.03 .XX .XXX +.015 +2 DO NOT SCALE THIS DRAWING 2 319 SERIES SWING ARM CLAMP SHIELD SOCK TERMINATION PROCEDURE APPROVED RELEASE DATE ORIGINAL RELEASE DATE CODE IDENT. NO. SIZE 06324 B/F 05-5368 P/C GAP NON REPAIRABLE COMMERCIAL ITEM SCALE N/A WEIGHT D GAP-027 N/A SHEET REV. 2 3 OF 3 1 of 1