GLENAIR GAP-027

WIRE BUNDLE
2
OVERALL BRAID
FROM BACKSHELL
2.00 MIN
FIGURE 1A
BRAID TRANSITION
ANGLE
687-207 SPLIT SHIELD SUPPORT RING
OPTIONAL TAPE WRAP 5
ASSEMBLE SWING ARM CLAMP TO DESIRED CONFIGURATION TIGHTENING SCREWS TO LOCK ARMS IN PLACE
(STRAIGHT, 45°, OR 90° CONFIGURATION) LEAVING SADDLE CLAMP HARDWARE LOOSE.
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
TEMPORARILY ASSEMBLE ADAPTER TO CONNECTOR (NOT SHOWN) AND PUSH BACK BACKSHELL BRAID.
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)
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)
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)
PIN CONNECTOR, SLIDE BACKSHELL FORWARD, AND HAND TIGHTEN BACKSHELL TO CONNECTOR.
1.
2.
3.
4.
5.
6.
7.
+
- 1/16
+.03
.XX
.XXX +
-.015
+ 2
-
B/F
05-5368 P/C
GAP
DO NOT SCALE THIS DRAWING
ANGLES
DECIMALS
FRACTIONS
TOLERANCES:
DIMENSIONS ARE IN INCHES
.38
2
APPROVED
NON REPAIRABLE COMMERCIAL ITEM
RELEASE DATE
ORIGINAL
RELEASE DATE
APPROVED
DETAIL-A
PIGTAIL
DATE
APPROVED
04/18/06
TMH
GAP-027
CAD 1991
C
SCALE
N/A
06324
WEIGHT
D
CODE IDENT. NO. SIZE
N/A
SHEET
GAP-027
2
1 of 1
1 OF 3
REV.
319 SERIES SWING ARM CLAMP
SHIELD SOCK TERMINATION
PROCEDURE
1211 AIR WAY - GLENDALE - CALIFORNIA 91201
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.
CAUTION:
TSP JACKET
TYING CORD
SOLDER SLEEVE
EXPOSED BRAID
SHRINK SLEEVE
DRAWN K. BAILEY 03/16/05
CHECK J. PLESSAS 03/16/05
ENGR J. PLESSAS 03/16/05
14
DESCRIPTION
REVISIONS
WINDOW STRIP
1.5/3.0
(OPTIONAL)
PRELIMINARY
WIRE
CONTACT
90° CONFIGURATION
UNLESS OTHERWISE SPECIFIED
SYM.
2
1.7/3.7
45° CONFIGURATION
JACKET (IF APPLICABLE)
OVERALL BRAID FROM
WIRE BUNDLE (IF APPLICABLE)
TAP WRAP UNDER RING
TO ENSURE SNUG FIT
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.
STEPS:
FIGURE 1
CONDUCTOR
OPTIONAL TAPE WRAP
STRAIGHT
CONFIGURATION
DETAIL-A
6.0/10.0
From the desk of James Plessas
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.
WRAP SHIELD SUPPORT RING ASSEMBLY WITH HIGH TEMPERATURE TAPE, USING 50% OVERLAP (NOT SHOWN).
10.
11.
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.
9.
FIGURE 3
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.
CONT'D
EQUALLY SPACE PIGTAILS
AROUND RING
FIGURE 2
STAGGER SOLDER
SLEEVES
LACING STRING OR
HIGH TEMPERATURE TY-STRAP
.50 APPROX.
CONDUCTORS
SUPPORT RING
B/F
05-5368 P/C
GAP
DO NOT SCALE THIS DRAWING
ANGLES
DECIMALS
+
- 1/16
+.03
.XX
.XXX +
-.015
+ 2
-
TOLERANCES:
DIMENSIONS ARE IN INCHES
SEE SHEET 1
DESCRIPTION
REVISIONS
2
APPROVED
NON REPAIRABLE COMMERCIAL ITEM
RELEASE DATE
ORIGINAL
RELEASE DATE
APPROVED
DRAWN K. BAILEY 03/16/05
CHECK J. PLESSAS 03/16/05
ENGR J. PLESSAS 03/16/05
DATE
CAD 1991
SCALE
N/A
06324
WEIGHT
D
CODE IDENT. NO. SIZE
N/A
SHEET
GAP-027
2
1 of 1
2 OF 3
REV.
319 SERIES SWING ARM CLAMP
SHIELD SOCK TERMINATION
PROCEDURE
C
APPROVED
GAP-027
1211 AIR WAY - GLENDALE - CALIFORNIA 91201
LACING STRING OR
HIGH TEMPERATURE TY-STRAP
FIGURE 4
UNLESS OTHERWISE SPECIFIED
FRACTIONS
SYM.
600-052
1.00 APPROX.
LACING STRING OR
HIGH TEMPERATURE TY-STRAP
8.
STEPS:
SHIELD
PIGTAIL
1.00 MAX
TUCK BRAID
AS SHOWN
From the desk of James Plessas
+
- 1/16
+.03
.XX
.XXX +
-.015
+ 2
-
B/F
05-5368 P/C
GAP
DO NOT SCALE THIS DRAWING
ANGLES
DECIMALS
FRACTIONS
TOLERANCES:
DIMENSIONS ARE IN INCHES
UNLESS OTHERWISE SPECIFIED
FIGURE 5
SUGGEST USING TEFLON TAPE WRAP OR M85049/127 BUSHING STRIP, AS NEEDED, TO CUSION BRAID SOCK UNDER
THE SADDLE CLAMPS.
SEE GLENAIR DRAWING 687-654, 687-655 & 687-656 FOR SADDLE BAR REPLACEMENT PARTS.
1.00 APPROX.
102-080 EXPANDO SLEEVE
BRAID SOCK
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.
15.
SYM.
2
APPROVED
NON REPAIRABLE COMMERCIAL ITEM
RELEASE DATE
ORIGINAL
RELEASE DATE
APPROVED
DESCRIPTION
REVISIONS
CAD 1991
SCALE
N/A
06324
WEIGHT
D
CODE IDENT. NO. SIZE
N/A
SHEET
GAP-027
2
1 of 1
3 OF 3
REV.
319 SERIES SWING ARM CLAMP
SHIELD SOCK TERMINATION
PROCEDURE
C
APPROVED
1211 AIR WAY - GLENDALE - CALIFORNIA 91201
DATE
GAP-027
LACE TIE, TAPE, OR SHRINK
SLEEVE MAY BE USED
TO DRESS ENDS
SEE SHEET 1
DRAWN K. BAILEY 03/16/05
CHECK J. PLESSAS 03/16/05
ENGR J. PLESSAS 03/16/05
LACING STRING OR HIGH TEMPERATURE TY-STRAPS
APPLIED IN 1.00 INCH INCREMENTS OPTIONAL
(LACING MUST BE PLACED OVER WINDOW STRIP AREA)
14.
SADDLE SCREW
4
4
6
6
6
6
6
6
6
-
ARM SCREW
INSTALLATION
TORQUE
(IN LB)
14
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)
ARM SCREW
4
4
6
6
6
6
6
6
6
-
SIZE
ARM SCREW
13.
4
4
6
6
6
6
6
6
6
6
10
10
SADDLE SCREW
INSTALLATION
TORQUE
(IN LB)
14
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
4
4
6
6
6
6
6
6
6
6
10
10
SIZE
SADDLE SCREW
12.
CONT'D
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
35
40
40
40
40
40
80
80
80
120
120
120
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
STEPS:
HEX COUPLING
TORQUE
WRENCH 13
COUPLING RING
INSTALLATION
TORQUE
(IN LB)
13
CONNECTOR
SHELL
SIZE
REF
TABLE I
From the desk of James Plessas