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Boeing 707 Wiring

Boeing 707 Wiring

Assembly of connectors with rear release contacts
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ASSEMBLY OF CONNECTORS WITH REAR RELEASE CONTACTS
PARAGRAPH
1.
GENERAL DATA
A.
Connector Assembly
2.
CONNECTOR DISASSEMBLY
A.
Contact Removal
B.
Contact Replacement
707, 727-787
STANDARD WIRING PRACTICES MANUAL
TABLE OF CONTENTS
D6-54446
ECCN 9E991 BOEING PROPRIETARY - See title page for details
PAGE
2
2
2
2
3
20-63-00
Page 1
Oct 15/2015

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  • Page 1 STANDARD WIRING PRACTICES MANUAL ASSEMBLY OF CONNECTORS WITH REAR RELEASE CONTACTS TABLE OF CONTENTS PARAGRAPH PAGE GENERAL DATA Connector Assembly CONNECTOR DISASSEMBLY Contact Removal Contact Replacement 20-63-00 Page 1 D6-54446 Oct 15/2015 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 2 Carefully pull the wire and the tool out of the contact cavity at the same time. If the removal tool does not release the contact from the contact cavity: Carefully pull the tool out of the contact cavity. 20-63-00 Page 2 D6-54446 Jun 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 3 Do Step 2.B.(3) through Step 2.B.(6) again. Assemble a new contact on the end of the wire. Refer to the applicable Subject for the connector. 20-63-00 Page 3 D6-54446 Jun 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...

  • Page 5: Table Of Contents

    PARAGRAPH PAGE PART NUMBERS AND DESCRIPTION Connector Part Numbers Contact Part Numbers CONNECTOR DISASSEMBLY Connector Disconnect Contact Removal CONNECTOR ASSEMBLY Contact Assembly Contact Insertion 20-63-01 Page 1 D6-54446 Feb 15/2016 ECCN 9E991 BOEING PROPRIETARY - See title page for details...

  • Page 6: Part Numbers And Description

    Contact Part Numbers Table 2 CONTACT PART NUMBERS Contact Size Contact Type Part Number Supplier Engaging End Crimp Barrel 0641-1-2031 Deutsch M39029/4-110 100503 Deutsch Socket M39029/5-115 20-63-01 Page 2 D6-54446 Feb 15/2016 ECCN 9E991 BOEING PROPRIETARY - See title page for details...

  • Page 7: Connector Disassembly

    Removal Tool Supplier M15570-20 Deutsch M81969/14-02 NAS1664-20 M15570-16 Deutsch M81969/14-03 NAS1664-16 M15570-12 Deutsch M81969/14-04 NAS1664-12 Make a selection of a removal tool from Table 3. 20-63-01 Page 3 D6-54446 Jun 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...

  • Page 8: Connector Assembly

    For size 16 and 12 contacts, remove ¼ in. (6.35 mm) ±1/32 in. (0.79 mm) of insulation. Make a selection of a crimp tool from Table 4. Insert the wire into the crimp barrel of the contact. 20-63-01 Page 4 D6-54446 Oct 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...

  • Page 9: Contact Insertion

    Insert the contact straight into the proper cavity until a slight click and resistance to further motion occur. Carefully withdraw the tool straight out of the contact cavity. 20-63-01 Page 5 D6-54446 Jun 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 11 Seal Plug or Seal Rod Installation CONNECTOR INSTALLATION Connection of the BACC63DE Plug and the BACC63DF Receptacle Connection of the BACC63DG Plug and BACC63DH Receptacle 20-63-02 Page 1 D6-54446 Jun 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...

  • Page 12: Part Numbers And Description

    BACC63DF() Receptacle Amphenol PCD BACC63DG() Plug Amphenol PCD BACC63DH() Receptacle Amphenol PCD 2448413 S00061547046_V1 BACC63DE PLUG AND BACC63DF RECEPTACLE PART NUMBER STRUCTURE Figure 1 20-63-02 Page 2 D6-54446 Oct 15/2015 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 13 • They have a quick disconnect latch configuration • The contacts are rear release, rear removable • The connectors have a color that shows the alternate keyway position. 20-63-02 Page 3 D6-54446 Oct 15/2015 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 14 BACC63DE, BACC63DF, BACC63DG, AND BACC63DH QUICK DISCONNECT CIRCULAR CONNECTORS 2446180 S00061546664_V1 BACC63DE PLUG AND BACC63DF RECEPTACLE CONFIGURATION Figure 3 2448416 S00061547048_V1 BACC63DG PLUG AND BACC63DH RECEPTACLE CONFIGURATION Figure 4 20-63-02 Page 4 D6-54446 Jun 15/2021 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 15 Contact Part Numbers 2449029 S00061546903_V1 STANDARD SIZE 1616, REAR RELEASE, CRIMP TYPE CONTACTS Figure 5 2446183 S00061544383_V1 EXAMPLE OF A CONTACT SIZE Figure 6 20-63-02 Page 5 D6-54446 Jun 15/2021 ECCN 9E991 BOEING PROPRIETARY - See title page for details...

  • Page 16: Contact Part Numbers

    CONTACT PART NUMBERS Contact Size Contact Type Boeing Standard Color Band Finish BACC47GC3A Blue Gold 1616 Socket BACC47GD3A Blue Gold BACC47GC2A Gold 2020 Socket BACC47GD2A Gold 20-63-02 Page 6 D6-54446 Oct 15/2015 ECCN 9E991 BOEING PROPRIETARY - See title page for details...

  • Page 17: Connector Disassembly

    Hold the two ends of the connector at the same time. Turn one end of the connector approximately 90 degrees. Pull the plug and receptacle apart. 20-63-02 Page 7 D6-54446 Oct 15/2015 ECCN 9E991 BOEING PROPRIETARY - See title page for details...

  • Page 18: Contact Removal

    TT-I-735 An available source Make a selection of a contact removal tool from Table 3. Refer to Figure 9 for contact removal tool configuration. 20-63-02 Page 8 D6-54446 Oct 15/2015 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 19 NOTE: To help removal of the contact, use the lubricant to lubricate the removal tool. Refer to Table 4. Hold the wire against the tool. Pull the tool and the wire out from the contact cavity. Refer to Figure 10. 20-63-02 Page 9 D6-54446 Oct 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...

  • Page 20: Seal Plug Removal

    Turn the removal tool approximately 90 degrees. Do Step 2.C.(2) through Step 2.C.(6) again. Seal Plug Removal Table 5 NECESSARY TOOL Tool Type Pliers Needle Nose 20-63-02 Page 10 D6-54446 Jun 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...

  • Page 21: Connector Assembly

    Assemble an insulated shield ground wire. Refer to Subject 20-10-15. Remove the unwanted length from the end of the shield ground wire and the wires of the cable. Refer to Figure 12. 20-63-02 Page 11 D6-54446 Oct 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...

  • Page 22: Cable Preparation

    • Subject 20-10-15 for the assembly of the shield ground wire that is not at the end of the cable jacket. Make sure that the shield ground wire is pointed in the direction that is specified for the shield ground wire connection. 20-63-02 Page 12 D6-54446 Oct 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...

  • Page 23: Increase Of The O.d. Of A Wire

    NOTE: If the location of a shield ground wire assembly prevents correct position of the sleeve, the length of the sleeve can be decreased. 20-63-02 Page 13 D6-54446 Oct 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 24 • The forward end of the sleeve is aligned with the end of the wire or 0.06 in. (1.52 mm) maximum from the end of the insulation. Refer to Figure 16. If more sleeves are specified, do Step 3.C.(1) through Step 3.C.(3) again. 20-63-02 Page 14 D6-54446 Oct 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...

  • Page 25: Contact Assembly

    Size Part Number Setting Supplier Part Number Color Block Supplier Color 612916 Balmar Blue Yellow M22520/1-01 M22520/1-04 2020 M22520/2-01 M22520/2-10 ST2220-1-Y Boeing ST2220-1-2 Boeing 20-63-02 Page 15 D6-54446 Oct 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 26 M22520/1-04 MS3191-1 11-7771-29 Amphenol ST2220-1-Y Boeing ST2220-1-2 Boeing 11148 Buchanan Blue 614019 Balmar Blue 1616 M22520/1-01 M22520/1-04 MS3191-1 11-7771-29 Amphenol ST2220-1-Y Boeing ST2220-1-2 Boeing 20-63-02 Page 16 D6-54446 Oct 15/2017 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 27 Make sure that: • All of the strands of the conductor are in the crimp barrel. Refer to Figure 20 20-63-02 Page 17 D6-54446 Oct 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 28 • The strands of the conductor can be seen in the inspection hole. Refer to Figure 21 for permitted conductor installation in inspection hole 2448421 S00061547063_V1 POSITION OF THE END OF THE CONDUCTOR IN THE INSPECTION HOLE Figure 21 20-63-02 Page 18 D6-54446 Oct 15/2015 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 29 MORE THAN 15 DEGREES CAN CAUSE DAMAGE TO THE WIRE. CAUTION Examine the contact assembly: Make sure that: • The crimp barrel has a full crimp compression. Refer to Figure 24 20-63-02 Page 19 D6-54446 Oct 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 30 NOTE: A compression that extends into the inspection hole is permitted if: • The crimp barrel around the inspection hole does not have a crack 20-63-02 Page 20 D6-54446 Jun 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...

  • Page 31: Contact Insertion

    Amphenol 11-8794-16 Amphenol Blue Metal M81969/8-07 1616 MS27495A16 RX16-4 Burndy M81969/14-03 Blue Plastic MS27534-16 A DEFECTIVE TOOL CAN CAUSE INJURY TO THE OPERATOR. WARNING 20-63-02 Page 21 D6-54446 Jun 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 32 POSITION OF THE WIRED CONTACT IN RELATION TO THE CONTACT CAVITY Figure 27 Push the tool straight into the contact cavity until the tool stops. Refer to Figure 28. 20-63-02 Page 22 D6-54446 Jun 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 33 PERFORMANCE AND RELIABILITY OF THE WIRE. CAUTION Lightly pull the wire to make sure that the contact is locked in the contact cavity. Refer to Figure 20-63-02 Page 23 D6-54446 Jun 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...

  • Page 34: Spare Contact Installation

    Axially align the tool and the contact. Push the tool straight into the contact cavity until the tool stops. Carefully remove the tool from the contact cavity. 20-63-02 Page 24 D6-54446 Jun 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...

  • Page 35: Seal Plug Or Seal Rod Installation

    Refer to Figure 30. 2446193 S00061546681_V1 POSITION OF THE KEYS AND THE KEYWAYS Figure 30 Push the plug into the receptacle until it stops. 20-63-02 Page 25 D6-54446 Jun 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...

  • Page 36: Connection Of The Bacc63Dg Plug And Bacc63Dh Receptacle

    Align the front ends of the plug and the receptacle. Refer to Figure 32. 2448417 S00061547070_V1 BACC63DE PLUG AND BACC63DF RECEPTACLE ASSEMBLY Figure 32 Push the plug straight into the receptacle until it stops. 20-63-02 Page 26 D6-54446 Jun 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 37 BACC63DE, BACC63DF, BACC63DG, AND BACC63DH QUICK DISCONNECT CIRCULAR CONNECTORS Twist each connector in opposite direction until the lock latches in the plug and the slots in the receptacle are fully engaged. 20-63-02 Page 27 D6-54446 Jun 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 39 Contact Assembly Preparation of a Wire that has an Oversize Insulation Diameter Increase the O.D. of an Unshielded Wire Contact Insertion Seal Plug Installation 20-63-03 Page 1 D6-54446 Oct 15/2017 ECCN 9E991 BOEING PROPRIETARY - See title page for details...

  • Page 40: Part Numbers And Description

    • They have a bayonet coupling • The contacts are rear release, rear removable • The connectors have a color that shows the alternate keyway position. 20-63-03 Page 2 D6-54446 Oct 15/2015 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 41 STANDARD WIRING PRACTICES MANUAL BACC63ED, BACC63EE AND BACC63EF MINIATURE CIRCULAR CONNECTORS 2449245 S00061547073_V1 BACC63ED STRAIGHT RECEPTACLE Figure 2 2449246 S00061547074_V1 BACC63EE PLUG Figure 3 20-63-03 Page 3 D6-54446 Oct 15/2015 ECCN 9E991 BOEING PROPRIETARY - See title page for details...

  • Page 42: Contact Part Numbers

    Orange Blue Yellow Gold BACC47GC3A Blue Gold NOTE: The size 2222D contact has a size 22 engaging end and a size 22 crimp barrel. 20-63-03 Page 4 D6-54446 Oct 15/2015 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 43 BACC63ED, BACC63EE AND BACC63EF MINIATURE CIRCULAR CONNECTORS 2448999 S00061545899_V1 M39029 REAR RELEASE CONTACTS Figure 5 2449029 S00061546903_V1 BACC47GC AND BACC47GD REAR RELEASE CONTACTS Figure 6 20-63-03 Page 5 D6-54446 Oct 15/2015 ECCN 9E991 BOEING PROPRIETARY - See title page for details...

  • Page 44: Insert Configurations

    NOTE: Figure 9 and Figure 10 show the rear face of an insert that has pins. The view of the rear face of an insert that has sockets is the mirror image of this view. 20-63-03 Page 6 D6-54446 Oct 15/2015 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 45 BACC63ED, BACC63EE AND BACC63EF MINIATURE CIRCULAR CONNECTORS 2449254 S00061547076_V1 SHELL SIZE A INSERT CONFIGURATIONS Figure 9 2449255 S00061547077_V1 SHELL SIZE B INSERT CONFIGURATIONS Figure 10 20-63-03 Page 7 D6-54446 Oct 15/2015 ECCN 9E991 BOEING PROPRIETARY - See title page for details...

  • Page 46: Connector Disassembly

    TT-I-735 An available source Make a selection of a contact removal tool from Table 4. Refer to Figure 11 for contact removal tool configuration. 20-63-03 Page 8 D6-54446 Oct 15/2015 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 47 Make sure that the tool stays aligned with the contact cavity. NOTE: To help removal of the contact, use the lubricant to lubricate the removal tool. Refer to Table 5. 20-63-03 Page 9 D6-54446 Jun 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...

  • Page 48: Contact Removal

    If the contact is not released from the connector: Pull the removal tool out of the contact cavity. Turn the removal tool approximately 90 degrees. 20-63-03 Page 10 D6-54446 Oct 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...

  • Page 49: Seal Plug Removal

    Remove 2.25 ±0.10 in. (57.15 ±2.54 mm) of the cable jacket from the end of the cable. Refer to: • Figure 14 • Subject 20-00-15 for the procedure to remove the cable jacket. 2449010 S00061547055_V1 CABLE JACKET REMOVAL Figure 14 20-63-03 Page 11 D6-54446 Oct 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...

  • Page 50: Contact Assembly

    Part Number Color Block Supplier Color M22520/2-01 M22520/2-09 M22520/2-01 M22520/2-09 WA22 Daniels M22520/2-09 2222D Socket M22520/2-01 M22520/2-06 Socket M22520/2-01 M22520/2-06 Socket WA22 Daniels M22520/2-06 20-63-03 Page 12 D6-54446 Oct 15/2017 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 51 Refer to Table 9. If the O.D. of the wire is larger than the maximum, use the procedure in Paragraph 4.C. to prepare the wire. 20-63-03 Page 13 D6-54446 Jun 15/2016 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 52 0.03 in. (0.76 mm) • The heat shrinkable sleeve makes an overlap on the wire insulation of 0.4 in. (10.16 mm) minimum. 20-63-03 Page 14 D6-54446 Oct 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...

  • Page 53: Preparation Of A Wire That Has An Oversize Insulation Diameter

    Remove a 1.00 ±0.06 in. (25.40 ±1.52 mm) length of insulation from the end of the wire. Refer to Figure 18. 2449249 S00061547081_V1 INSULATION REMOVAL LENGTH Figure 18 20-63-03 Page 15 D6-54446 Oct 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...

  • Page 54: Increase The O.d. Of An Unshielded Wire

    Contact Insertion Table 11 CONTACT INSERTION TOOLS Insertion Tool Contact Size Color Material Part Number Supplier Green Plastic M81969/14-01 2222D Metal M81969/8-01 20-63-03 Page 16 D6-54446 Oct 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 55 Put the wired contact into the insertion tool. Refer to Figure 20. Make sure that the tip of the tool is against the end of the wire barrel of the contact. 20-63-03 Page 17 D6-54446 Jun 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 56 Make sure that the insertion tool stays aligned with the contact cavity. 2449252 S00061547079_V1 INSERTION OF THE CONTACT Figure 22 Carefully remove the tool from the contact cavity. 20-63-03 Page 18 D6-54446 Jun 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 57 If the contact is not locked in the contact cavity: Pull the wired contact out of the contact cavity. Do Step 4.E.(2) through Step 4.E.(6) again. 20-63-03 Page 19 D6-54446 Jun 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...

  • Page 58: Seal Plug Installation

    Make sure that the distance from the connector grommet to the cut end of the seal plug is between 0.1 in. (2.54 mm) and 0.2 in. (5.08 mm). 20-63-03 Page 20 D6-54446 Oct 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 59 Increase of the O.D. of a Wire - Unshielded Wire and Cable, Firewall Leakage Configuration Contact Assembly Contact Insertion Seal of an Empty Contact Cavity Backshell and Strain Relief Assembly 20-63-13 Page 1 D6-54446 Oct 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...

  • Page 60: Paragraph Page

    STANDARD WIRING PRACTICES MANUAL ASSEMBLY OF MIL-C-83723 SERIES III TYPE CONNECTORS PARAGRAPH PAGE CONNECTOR INSTALLATION Connector Installation INSTALLATION OF CONNECTOR CAPS Installation of a Receptacle Cap 20-63-13 Page 2 D6-54446 Oct 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...

  • Page 61: General Data

    0.040 BACC63BT MIL-C-83723 Series III type 0.053 0.096 0.040 BACC63CM ESC 10 Class SE 0.053 0.096 0.040 BACC63CN ESC 10 Class SE 0.053 0.096 20-63-13 Page 3 D6-54446 Oct 15/2015 ECCN 9E991 BOEING PROPRIETARY - See title page for details...

  • Page 62: Maximum Wire O

    0.103 0.151 0.078 BACC63CN ESC 10 Class SE 0.103 0.151 0.078 M83723/( ) MIL-C-83723 Series III 0.103 0.151 R073510A06SN-200 MIL-C-83723 Series III type 0.078 20-63-13 Page 4 D6-54446 Feb 15/2017 ECCN 9E991 BOEING PROPRIETARY - See title page for details...

  • Page 63: Part Numbers And Description

    APPROVED SUPPLIERS OF BOEING STANDARD CONNECTORS Boeing Standard Supplier ITT Cannon UK BACC63BR() Matrix Pyle-National ITT Cannon UK BACC63BT() Matrix Pyle-National Deutsch Matrix BACC63CM() Pyle-National Souriau 20-63-13 Page 5 D6-54446 Jun 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...

  • Page 64: Bacc63Br And Bacc63Bt Thread Coupled Firewall Connectors

    BACC63BR and BACC63BT Thread Coupled Firewall Connectors The BACC63BR and BACC63BT connectors have a self-locking coupling mechanism. 2446295 S00061547087_V1 BOEING BACC63BR AND BACC63BT CONNECTOR PART NUMBER STRUCTURE Figure 1 20-63-13 Page 6 D6-54446 Feb 15/2017 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 65 ITT CANNON BACC63BR AND BACC63BT CONNECTOR PART NUMBER STRUCTURE - HTBMF Figure 2 2446301 S00061547089_V1 MATRIX BACC63BR AND BACC63BT CONNECTOR PART NUMBER STRUCTURE - MT Figure 3 20-63-13 Page 7 D6-54446 Feb 15/2017 ECCN 9E991 BOEING PROPRIETARY - See title page for details...

  • Page 66: Bacc63Cm And Bacc63Cn Thread Coupled Firewall Connectors

    • Have the performance of the British Aerospace Companies Standard ESC 10 Class SE plug and Class KE receptacle. 2446296 S00061547091_V1 BOEING BACC63CM AND BACC63CN CONNECTOR PART NUMBER STRUCTURE Figure 5 20-63-13 Page 8 D6-54446 Feb 15/2017 ECCN 9E991 BOEING PROPRIETARY - See title page for details...

  • Page 67: Matrix 527() Connectors

    MATRIX 52752-() CONNECTOR PART NUMBER STRUCTURE Figure 6 2446299 S00061547093_V1 MATRIX 52753-() CONNECTOR PART NUMBER STRUCTURE Figure 7 2446300 S00061547094_V1 MATRIX 52761-() CONNECTOR PART NUMBER STRUCTURE Figure 8 20-63-13 Page 9 D6-54446 Feb 15/2017 ECCN 9E991 BOEING PROPRIETARY - See title page for details...

  • Page 68: Mil-C-83723 Series Iii Connectors

    MIL-C-83723 Series III Connectors MIL-C-83723 Series III connectors can be Type T Threaded, or Type B Bayonet coupling. 2448254 S00061547095_V1 M83723 CONNECTOR PART NUMBER STRUCTURE Figure 9 20-63-13 Page 10 D6-54446 Feb 15/2017 ECCN 9E991 BOEING PROPRIETARY - See title page for details...

  • Page 69: Rms R0735( )A( ) Bayonet Coupled, Flange Mount Receptacle

    N = Normal 6, 7, 8, 9 or 10 are the Alternate Keyway Positions 2563831 S0000612825_V1 RMS R0735( )A( ) CONNECTOR PART NUMBER STRUCTURE Figure 10 20-63-13 Page 11 D6-54446 Feb 15/2017 ECCN 9E991 BOEING PROPRIETARY - See title page for details...

  • Page 70: Amphenol Special Audio Connector

    Amphenol Special Audio Connector The Amphenol special audio receptacle connector has 10 size 16 standard socket contacts. 2446303 S00061547096_V1 AMPHENOL 10-584762 RECEPTACLE CONNECTOR Figure 11 20-63-13 Page 12 D6-54446 Jun 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...

  • Page 71: Contact Part Numbers

    ASSEMBLY OF MIL-C-83723 SERIES III TYPE CONNECTORS Contact Part Numbers 2449029 S00061546903_V1 BOEING STANDARD CONTACTS Figure 12 2446651 S00061545900_V1 EXAMPLE OF A CONTACT SIZE Figure 13 20-63-13 Page 13 D6-54446 Jun 15/2021 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 72 BACC47ES3 Yellow Socket BACC47ET3 Yellow Table 7 APPROVED SUPPLIERS OF BOEING STANDARD CONTACTS Boeing Standard Supplier Amphenol BACC47ES() Pyle-National Tri-Star Amphenol BACC47ET() Pyle-National Tri-Star 20-63-13 Page 14 D6-54446 Feb 15/2021 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 73 Contact Size Contact Type Contact Part Number Supplier Engaging End Crimp Barrel Alumel 5000-070-120 Matrix Chromel 5000-070-220 Matrix Alumel 5100-108-120 Matrix Socket Chromel 5100-108-220 Matrix 20-63-13 Page 15 D6-54446 Jun 15/2017 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 74 Figure 17 10-6 or 10-06 Figure 17 12-3 or 12-03 Figure 18 12-12 Figure 18 14-4 or 14-04 Figure 19 14-7 or 14-07 Figure 19 20-63-13 Page 16 D6-54446 Jun 15/2017 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 75 NOTE: Figure 16 through Figure 25 show the front face of an insert that has sockets. The view of the front face of an insert that has pins is the mirror image of this view. 20-63-13 Page 17 D6-54446 Jun 15/2017 ECCN 9E991 BOEING PROPRIETARY - See title page for details...

  • Page 76: Insert Configurations

    ASSEMBLY OF MIL-C-83723 SERIES III TYPE CONNECTORS 2446304 S00061547097_V1 8-() INSERT CONFIGURATIONS Figure 16 2446305 S00061547098_V1 10-() INSERT CONFIGURATIONS Figure 17 2446306 S00061547099_V1 12-() INSERT CONFIGURATIONS Figure 18 20-63-13 Page 18 D6-54446 Jun 15/2017 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 77 STANDARD WIRING PRACTICES MANUAL ASSEMBLY OF MIL-C-83723 SERIES III TYPE CONNECTORS 2446307 S00061547100_V1 14-() INSERT CONFIGURATIONS Figure 19 2446308 S00061547101_V2 16-() INSERT CONFIGURATIONS Figure 20 20-63-13 Page 19 D6-54446 Jun 15/2017 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 78 STANDARD WIRING PRACTICES MANUAL ASSEMBLY OF MIL-C-83723 SERIES III TYPE CONNECTORS 2446309 S00061547102_V1 18-() INSERT CONFIGURATIONS Figure 21 2446310 S00061547103_V1 20-() INSERT CONFIGURATIONS Figure 22 20-63-13 Page 20 D6-54446 Jun 15/2017 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 79 STANDARD WIRING PRACTICES MANUAL ASSEMBLY OF MIL-C-83723 SERIES III TYPE CONNECTORS 2446311 S00061547104_V1 22-() INSERT CONFIGURATIONS Figure 23 2446312 S00061547105_V1 24-() INSERT CONFIGURATIONS Figure 24 20-63-13 Page 21 D6-54446 Jun 15/2017 ECCN 9E991 BOEING PROPRIETARY - See title page for details...

  • Page 80: Connector Disassembly

    Hold the end of the seal plug or the seal rod tightly in the jaws of the pliers. Pull the seal plug or the seal rod from the contact cavity. 20-63-13 Page 22 D6-54446 Oct 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...

  • Page 81: Contact Removal

    At the rear of the connector, put the removal tool on the wire. Axially align the tool and the contact cavity at the rear of the connector. 20-63-13 Page 23 D6-54446 Jun 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...

  • Page 82: Unwired Contact Removal

    DO NOT USE MORE THAN THE NECESSARY AMOUNT OF FORCE TO PUSH THE TOOL INTO THE CONTACT CAVITY. DAMAGE TO THE CONTACT RETENTION CLIPS CAN OCCUR. CAUTION 20-63-13 Page 24 D6-54446 Jun 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...

  • Page 83: Connector Assembly

    0.19 ±0.03 0.19 ±0.03 0.50 ±0.03 Fold the conductor back. 0.19 ±0.03 0.25 ±0.03 0.25 ±0.03 0.25 ±0.03 0.50 ±0.03 Fold the conductor back. 20-63-13 Page 25 D6-54446 Jun 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 84 • Paragraph 5.C. for the procedure to increase the O.D. of an unshielded wire. If it is specified in Table 14, fold the conductor back on itself. Refer to: • Table 14 20-63-13 Page 26 D6-54446 Jun 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 85 ASSEMBLY OF MIL-C-83723 SERIES III TYPE CONNECTORS • Figure 27. 2446657 S00061544480_V1 FOLDED BACK CONDUCTOR Figure 27 Assemble the contact. Refer to Paragraph 5.M. 20-63-13 Page 27 D6-54446 Jun 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...

  • Page 86: Increase Of The O.d. Of The Wire - Shielded Wire

    0.75 ±0.10 in. (19.05 ±2.54 mm) length of the shield dead end sleeve on the cable. Cut the necessary length of the buildup sleeve. Make sure that: 20-63-13 Page 28 D6-54446 Oct 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 87 For a solder sleeve shield termination that is not at the end of the cable jacket, install the outer shield dead end sleeve. Refer to Figure 30. 20-63-13 Page 29 D6-54446 Oct 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 88 • The forward end of the shield dead end sleeve is 0.25 in. (6.35 mm) to 0.50 in. (12.7 mm) from the end of the shield. 20-63-13 Page 30 D6-54446 Oct 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...

  • Page 89: Increase Of The O.d. Of The Wire - Unshielded Wire

    Push the seal sleeve forward until the forward end of the seal sleeve makes a 0.25 in. (6.35 mm) to 0.50 in. (12.7 mm) overlap with the rear end of the buildup sleeve. 20-63-13 Page 31 D6-54446 Oct 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...

  • Page 90: Decrease Of The O.d. Of The Wire

    Make sure that this outer sleeve has the smallest diameter that will fit over the insulation of the wire. Remove 1.55 ±0.03 in. (39.37 ±0.76 mm) of insulation from the end of the wire. Refer to Figure 33. 20-63-13 Page 32 D6-54446 Oct 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...

  • Page 91: Preparation Of Champlain 24-00033 And Champlain 24-00034 Wire

    Refer to Figure 34. Make a selection of a heat shrinkable sleeve from Table 15. NOTE: For alternative heat shrinkable sleeves, refer to Subject 20-00-11. 20-63-13 Page 33 D6-54446 Oct 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...

  • Page 92: Preparation Of Rockbestos Or Cerro H22-4000 Wire

    Table 16 NECESSARY MATERIALS Size Material Part Number Supplier (inch) AMS-DTL-23053/12 Class 5 Available source Sleeve, Heat Shrinkable TFE-4X Chemplast TFE-4X Zeus Industrial Products 20-63-13 Page 34 D6-54446 Oct 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 93 • The distance from the forward end of the sleeve to the end of the inner insulation is not more than 0.13 in. (3.30 mm). Shrink the sleeve into its position. Refer to Subject 20-10-14. 20-63-13 Page 35 D6-54446 Oct 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 94 Shrink the sleeve into its position. Refer to Subject 20-10-14. Fold the conductor back on itself. NOTE: When the conductor is folded back on itself, the size of the conductor becomes 18 AWG. 20-63-13 Page 36 D6-54446 Oct 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...

  • Page 95: Preparation Of Specialty Cable 852-4985339 Cable Wire

    • The sleeve makes an overlap of approximately 0.5 in. (12.7 mm) with the insulation. Shrink the sleeve into its position. Refer to Subject 20-10-14. 20-63-13 Page 37 D6-54446 Oct 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...

  • Page 96: Preparation Of Bms 13-67 Type 2, Class 1 Cable (Wire Type Code 9U) For Termination In A Bacc63Cm Or Cn Connector

    • Subject 20-10-14 • Figure 38. Make sure that the end of the sleeve is aligned with the end of the inner layer of insulation. 20-63-13 Page 38 D6-54446 Oct 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...

  • Page 97: Preparation Of Bms 13-67 Type 2, Class 1 Cable (Wire Type Code 9U) For Termination In A Bacc63Cm Or Cn Connector With A Shield Ground Wire

    0.25 in. (6.35 mm) to 0.35 in. (8.89 mm). Assemble a shield ground wire shield termination with mechanical ferrules. Refer to: • Subject 20-10-15 20-63-13 Page 39 D6-54446 Oct 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 98 Make sure that the end of the sleeve is aligned with the end of the inner layer of insulation. 2449193 S00061547119_V1 POSITION OF THE SHIELD TERMINATION FERRULES AND THE HEAT SHRINKABLE SLEEVE Figure 40 20-63-13 Page 40 D6-54446 Oct 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...

  • Page 99: Increase Of The O.d. Of A Wire - Shielded Cable, Firewall Leakage Configuration

    Shield Dead End 2449542 S00061547120_V1 POSITION OF THE SLEEVES ON THE WIRE - SHIELD TERMINATION AT THE END OF THE CABLE JACKET Figure 41 20-63-13 Page 41 D6-54446 Jun 15/2021 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 100 • For a solder sleeve that is not at the end of the cable jacket, the distance from the rear end of the sleeve to the end of the shield is not more than 0.12 in. (3.05 mm). 20-63-13 Page 42 D6-54446 Oct 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 101 For a solder sleeve shield termination that is not at the end of the cable jacket, install the shield dead end sleeve. Refer to Figure 43. 20-63-13 Page 43 D6-54446 Oct 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 102 Table 20 HEAT SHRINKABLE SLEEVE TYPES Sleeve Type D-150-C-12 Seal Sleeve, Inner and Outer M23053/12 Build-Up 20-63-13 Page 44 D6-54446 Oct 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...

  • Page 103: Increase Of The O.d. Of A Wire - Unshielded Wire And Cable, Firewall Leakage Configuration

    • The rear end of the inner sleeve does not extend more than 0.1 in. (2.54 mm) from the rear end of the build-up sleeve. NOTE: An air pocket between the outer seal sleeve and the build-up sleeve is permitted. 20-63-13 Page 45 D6-54446 Oct 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...

  • Page 104: Contact Assembly

    WA22LC Daniels Daniels ST2220-1-Y Boeing ST2220-1-1 Boeing MS3191-1 MS3191-20A 11148 Fixed Buchanan Red Black M22520/1-01 M22520/1-02 Blue Blue WA27F Daniels TH1A Blue Blue Daniels 20-63-13 Page 46 D6-54446 Oct 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 105 Push the heat shrinkable sleeve forward until the forward end of the sleeve is 0.03 in. (0.76 mm) maximum from the end of the crimp barrel. Refer to Figure 45. 20-63-13 Page 47 D6-54446 Oct 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 106 Push the inner sleeve forward until the forward end of the sleeve is 0.03 in. (0.76 mm) maximum from the end of the crimp barrel. Refer to Figure 46. 2449093 S00061547125_V1 POSITION OF THE INNER HEAT SHRINKABLE SLEEVE Figure 46 20-63-13 Page 48 D6-54446 Oct 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...

  • Page 107: Contact Insertion

    NOTE: If a backshell is specified, the necessary backshell components must be installed on the wire harness before the insertion of the contacts into the connector. Refer to Paragraph 5.P. 20-63-13 Page 49 D6-54446 Oct 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 108 DO NOT USE MORE THAN THE NECESSARY AMOUNT OF FORCE TO PUSH THE TOOL INTO THE CONTACT CAVITY. DAMAGE TO THE CONTACT RETENTION CLIPS CAN OCCUR. CAUTION 20-63-13 Page 50 D6-54446 Oct 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...

  • Page 109: Seal Of An Empty Contact Cavity

    Tighten the cap with the hand until it stops. Make sure that: The cap and the receptacle are fully engaged. The cap cannot be turned more with the hand. 20-63-13 Page 51 D6-54446 Oct 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 111 Contact Part Numbers INSERT CONFIGURATIONS MIL-C-5015 Series Connectors CONNECTOR DISASSEMBLY Contact Removal CONNECTOR ASSEMBLY Wire Preparation Contact Assembly Contact Insertion Spare Contact and Seal Plug Installation 20-63-14 Page 1 D6-54446 Jun 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...

  • Page 112: General Data

    Refer to Table 4 for the applicable 71550SE-12T-03SN-960 Hi-Rel contacts for these connectors 892() Souriau 9440() Matrix 9446() Matrix 9816() Matrix MS3450() MS3452() MS3454() MS3456() MS3459() 20-63-14 Page 2 D6-54446 Oct 15/2015 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 113 2446315 S00061547128_V1 MATRIX 42250 AND 42839 SERIES CONNECTOR PART NUMBER STRUCTURE Figure 1 2446316 S00061547129_V1 SOURIAU 892 SERIES CONNECTOR PART NUMBER STRUCTURE Figure 2 20-63-14 Page 3 D6-54446 Oct 15/2015 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 114 2446317 S00061547130_V1 MATRIX 944 SERIES CONNECTOR PART NUMBER STRUCTURE Figure 3 2443661 S00061547131_V2 MS3450 THROUGH MS3459 MIL-C-5015 REAR RELEASE CONNECTOR PART NUMBER STRUCTURE Figure 4 20-63-14 Page 4 D6-54446 Oct 15/2021 ECCN 9E991 BOEING PROPRIETARY - See title page for details...

  • Page 115: Contact Part Numbers

    Supplier Barrel Size Size 5100-033-16-1 Matrix 5100-179-16-1 Socket 8950-5052A Souriau M39029/30-217 5000-029-16 Matrix BACC47GE1A Boeing M39029/29-212 5100-033-16-2 Matrix 8950-5053A Souriau Socket BACC47GF1A Boeing M39029/30-218 20-63-14 Page 5 D6-54446 Jun 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 116 NOTE: The contact part numbers in Table 4 are intended for Hi-Rel connectors only. Table 4 CONTACT PART NUMBERS FOR HI-REL CONNECTORS Connector Part Number Contact Part Number Contact Size Supplier 71550SE-12T-03SN-960 0012-136-004 Hi-Rel 44267KS-10SL-3BN-745 0012-217-016S Hi-Rel 20-63-14 Page 6 D6-54446 Feb 15/2016 ECCN 9E991 BOEING PROPRIETARY - See title page for details...

  • Page 117: Insert Configurations

    CONNECTOR ASSEMBLY Wire Preparation Table 6 INSULATION REMOVAL LENGTH Removal Length (inch) Crimp Barrel Size Special Instructions Target Tolerance 0.28 ±0.03 0.28 ±0.03 0.50 ±0.06 20-63-14 Page 7 D6-54446 Feb 15/2016 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 118 If the O.D. of the wire is less than the minimum seal diameter of the connector grommet holes, or if it is specified, increase the O.D. of the wire. Refer to Paragraph 1.A. 20-63-14 Page 8 D6-54446 Oct 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...

  • Page 119: Contact Assembly

    M22520/1-01 M22520/1-02 Blue M22520/1-01 M22520/1-02 Blue MS3191-1 MS3191-16A Blue ST2220-1-Y ST2220-1-2 WA27F M22520/1-02 Blue 294-126 M22520/1-01 M22520/1-02 Yellow MS3191-1 MS3191-12A Yellow WA27F M22520/1-02 Yellow 20-63-14 Page 9 D6-54446 Feb 15/2016 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 120 M22520/23-01 M22520/23-05 M22520/23-13 Table 8 CONTACT CRIMP TOOL SUPPLIERS Crimp Tool Supplier 11738 Thomas & Betts 13642 Thomas & Betts 294-126 Amphenol 400B Pico 20-63-14 Page 10 D6-54446 Jun 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 121 Put the filler wire in the crimp barrel of the contact. Put the conductor in the crimp barrel. Refer to Figure 7. Make sure that: 20-63-14 Page 11 D6-54446 Jun 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 122 If the contact has a filler wire, remove the unwanted length of the filler wire as close as possible to the end of the crimp barrel. Refer to Figure 8. 20-63-14 Page 12 D6-54446 Jun 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...

  • Page 123: Contact Insertion

    Matrix MS3165-4 6500-018-0 Matrix MS3165-0 Make a selection of contact insertion tool from Table 9. Put the wired contact into the applicable contact cavity. 20-63-14 Page 13 D6-54446 Jun 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...

  • Page 124: Spare Contact And Seal Plug Installation

    ASSEMBLY OF MIL-C-5015 TYPE CONNECTORS WITH REAR RELEASE CONTACTS Spare Contact and Seal Plug Installation All contact cavities that are not used must be sealed. Refer to Subject 20-60-08. 20-63-14 Page 14 D6-54446 Jun 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 125 STANDARD WIRING PRACTICES MANUAL ASSEMBLY OF MIL-C-81511 SERIES 1 AND SERIES 2 CONNECTORS TABLE OF CONTENTS PARAGRAPH PAGE ASSEMBLY OF MIL-C-81511 SERIES 1 AND SERIES 2 CONNECTORS 20-63-18 Page 1 D6-54446 Oct 15/2015 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 126 ASSEMBLY OF MIL-C-81511 SERIES 1 AND SERIES 2 CONNECTORS ASSEMBLY OF MIL-C-81511 SERIES 1 AND SERIES 2 CONNECTORS This Subject is now located in Subject 20-61-30. 20-63-18 Page 2 D6-54446 Oct 15/2015 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 127 Contact Insertion Installation of Size 8 Quadrax Contacts Spare Contact and Seal Plug Installation PLUG AND RECEPTACLE CONNECTION Connection of the Plug and the Receptacle 20-63-19 Page 1 D6-54446 Jun 15/2021 ECCN 9E991 BOEING PROPRIETARY - See title page for details...

  • Page 128: General Data

    CONNECTOR AFTER THE PLUG AND RECEPTACLE ARE FULLY MATED. IT IS SATISFACTORY TO USE A PLUG THAT HAS DAMAGE IN SERVICE UP TO 100 FLIGHT CYCLES. 20-63-19 Page 2 D6-54446 Jun 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...

  • Page 129: Connector Part Numbers

    Metal Shell, with Quadrax Contact Amphenol Metal Shell, with Standard Contact, Aluminum TVS06RF-15-4S Amphenol Shell Filter Connector, Insert Configuration 13-35 21-901034-005 Amphenol (SEE NOTE ) 20-63-19 Page 3 D6-54446 Jun 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 130 Amphenol Breech D38999/46 EMI Grounding, Metric Coupling Plug Breech Coupling D38999/49 In-Line Cable, Metric Receptacle NOTE: 21-901034-005 requires no sealing plug for unused cavities. 20-63-19 Page 4 D6-54446 Jun 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 131 2446323 S00061547137_V2 MIL-C-38999 SERIES I AND II CONNECTOR PART NUMBER STRUCTURE - MS27466 Figure 1 2446324 S00061547138_V1 D38999 CONNECTOR PART NUMBER STRUCTURE Figure 2 20-63-19 Page 5 D6-54446 Oct 15/2017 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 132 2449541 S00061547139_V1 D38999/33 PROTECTIVE THREADED RECEPTACLE CAP PART NUMBER STRUCTURE Figure 3 2449180 S00061547140_V1 HIREL 59300F AND 59300K CONNECTOR PART NUMBER STRUCTURE Figure 4 20-63-19 Page 6 D6-54446 Jun 15/2017 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 133 ASSEMBLY OF MIL-C-38999 CONNECTORS 2448315 S00061547141_V1 SOURIAU 8D CONNECTOR PART NUMBER STRUCTURE Figure 5 2448316 S00061547142_V1 BACC63CT AND BACC63CU CONNECTOR PART NUMBER STRUCTURE Figure 6 20-63-19 Page 7 D6-54446 Jun 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 134 RF = Nickel Aluminum RQW = Quadrax Contact, Shell Size Cadmium Finish 2449141 S00061547145_V2 AMPHENOL TV ( ) CONNECTOR PART NUMBER STRUCTURE Figure 8 20-63-19 Page 8 D6-54446 Jun 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...

  • Page 135: Contact Part Numbers

    ASSEMBLY OF MIL-C-38999 CONNECTORS 2449860 S00061547146_V1 Amphenol 10-695() Type Connector Part Number Structure Figure 9 Contact Part Numbers 2449029 S00061546903_V1 BOEING STANDARD CONTACTS Figure 10 20-63-19 Page 9 D6-54446 Jun 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 136 Socket BACC47GD2A Long BACC47GC3A Blue 1616 Socket BACC47GD3A Long Blue BACC47GC4A Yellow 1212 Socket BACC47GD4A Long Yellow BACC47GC6A Blue-Black 1614 Socket BACC47GD6A Long Blue-Black 20-63-19 Page 10 D6-54446 Oct 15/2021 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 137 Engaging End Crimp Barrel Band Color Orange Blue M39029/58-361 Brown Orange Socket, long Yellow M39029/56-349 White Orange Blue M39029/58-360 Black Orange Socket, long Yellow M39029/56-348 Gray 20-63-19 Page 11 D6-54446 Jun 15/2021 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 138 Yellow Orange Socket, long Green M39029/56-352 Orange Blue M39029/58-365 Green Orange Socket, long Green M39029/56-353 Orange Green M39029/58-528 Gray Green Socket, long M39029/56-527 Violet 20-63-19 Page 12 D6-54446 Jun 15/2021 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 139 Crimp Barrel Band Color Orange Blue M39029/58-361 Brown Orange Socket, short Green M39029/57-355 Green Orange Blue M39029/58-360 Black Orange Socket, short Green M39029/57-354 Yellow 20-63-19 Page 13 D6-54446 Jun 15/2021 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 140 Socket, short Green M39029/57-357 Violet Orange Blue M39029/58-364 Yellow Orange Socket, short Green M39029/57-358 Gray Orange Blue M39029/58-365 Green Orange Socket, short Green M39029/57-359 White 20-63-19 Page 14 D6-54446 Jun 15/2021 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 141 Table 8 SUPERSEDED CONTACT PART NUMBERS Superseded Contact New Contact Part Number Supplier Part Number Supplier MS27490-22D M39029/56-348 MS27490-22M M39029/56-349 MS27490-22 M39029/56-350 MS27490-20 M39029/56-351 20-63-19 Page 15 D6-54446 Jun 15/2021 ECCN 9E991 BOEING PROPRIETARY - See title page for details...

  • Page 142: Coax Contact Part Numbers And Components

    Coax Contact Part Numbers and Components Table 9 COAX CONTACT PART NUMBERS Contact Size Type Part Number Supplier Reference Socket 21-33101-37 Amphenol Figure 13 21-33102-37 Amphenol Figure 14 20-63-19 Page 16 D6-54446 Jun 15/2021 ECCN 9E991 BOEING PROPRIETARY - See title page for details...

  • Page 143: Necessary Parts

    21-33101-37 COAX SOCKET CONTACT COMPONENTS Figure 13 2449297 S00061547148_V1 21-33102-37 COAX PIN CONTACT COMPONENTS Figure 14 2449298 S00061547149_V1 AMPHENOL 10-452952 SEAL BOOT Figure 15 20-63-19 Page 17 D6-54446 Jun 15/2021 ECCN 9E991 BOEING PROPRIETARY - See title page for details...

  • Page 144: Quadrax Contact Part Numbers

    QUADRAX CONTACT PART NUMBERS FOR MIL-DTL-38999 SERIES III CONNECTORS Contact Size Type Boeing Standard BACC47GM1 Socket BACC47GN1 2448164 S00061547150_V1 COMPONENTS OF THE QUADRAX PIN CONTACT Figure 16 20-63-19 Page 18 D6-54446 Jun 15/2021 ECCN 9E991 BOEING PROPRIETARY - See title page for details...

  • Page 145: Insert Configurations

    707, 727-787 STANDARD WIRING PRACTICES MANUAL ASSEMBLY OF MIL-C-38999 CONNECTORS 2448165 S00061547151_V1 COMPONENTS OF THE QUADRAX SOCKET CONTACT Figure 17 Table 12 SUPPLIER PART NUMBERS FOR BOEING STANDARD SIZE 8 QUADRAX CONTACTS Alternative Contact Boeing Standard Part Number Supplier BACC47GM1 670175011...
  • Page 146 Figure 27 21-35 Figure 27 21-39 Figure 27 21-41 Figure 27 21-75 Figure 27 21-76 Figure 30 8 Quadrax 21-84 8 Quadrax Figure 30 20-63-19 Page 20 D6-54446 Jun 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 147 NOTE: Figure 18 through Figure 30 show the rear face of an insert that has sockets. The view of the rear face of an insert that has pins is the mirror image of this view. 2446325 S00061547152_V1 9-() INSERT CONFIGURATIONS Figure 18 20-63-19 Page 21 D6-54446 Jun 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 148 STANDARD WIRING PRACTICES MANUAL ASSEMBLY OF MIL-C-38999 CONNECTORS 11-98 11-5 11-35 2446326 S00061547153_V2 11-() INSERT CONFIGURATIONS Figure 19 2449535 S00061547154_V1 13-() INSERT CONFIGURATIONS Figure 20 20-63-19 Page 22 D6-54446 Jun 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 149 707, 727-787 STANDARD WIRING PRACTICES MANUAL ASSEMBLY OF MIL-C-38999 CONNECTORS 2449134 S00061547155_V1 14-() INSERT CONFIGURATIONS Figure 21 2446327 S00061547156_V1 15-() INSERT CONFIGURATIONS Figure 22 20-63-19 Page 23 D6-54446 Oct 15/2015 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 150 707, 727-787 STANDARD WIRING PRACTICES MANUAL ASSEMBLY OF MIL-C-38999 CONNECTORS 2449135 S00061547157_V1 16-() INSERT CONFIGURATIONS Figure 23 2446328 S00061547158_V1 17-() INSERT CONFIGURATIONS Figure 24 20-63-19 Page 24 D6-54446 Oct 15/2015 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 151 707, 727-787 STANDARD WIRING PRACTICES MANUAL ASSEMBLY OF MIL-C-38999 CONNECTORS 2447877 S00061547159_V1 18-() INSERT CONFIGURATIONS Figure 25 2446329 S00061547160_V1 19-() INSERT CONFIGURATIONS Figure 26 20-63-19 Page 25 D6-54446 Oct 15/2015 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 152 707, 727-787 STANDARD WIRING PRACTICES MANUAL ASSEMBLY OF MIL-C-38999 CONNECTORS 2446330 S00061547161_V2 21-() INSERT CONFIGURATIONS Figure 27 20-63-19 Page 26 D6-54446 Jun 15/2017 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 153 707, 727-787 STANDARD WIRING PRACTICES MANUAL ASSEMBLY OF MIL-C-38999 CONNECTORS 2446331 S00061547162_V1 23-() INSERT CONFIGURATIONS Figure 28 20-63-19 Page 27 D6-54446 Jun 15/2017 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 154 707, 727-787 STANDARD WIRING PRACTICES MANUAL ASSEMBLY OF MIL-C-38999 CONNECTORS 2443688 S00061547163_V1 25-() INSERT CONFIGURATIONS Figure 29 20-63-19 Page 28 D6-54446 Jun 15/2017 ECCN 9E991 BOEING PROPRIETARY - See title page for details...

  • Page 155: Connector Disassembly

    Metal DRK225-22 Daniels Plastic M81969/16-04 White 11-8675-24 Bendix 11-8795-24 Bendix ATBX2052 Astro Metal M81969/8-02 MS27495R22M RX24-3 Burndy 10-296943-23 Bendix M81969/14-01 Plastic White MS27509R22M MS27534-22D 20-63-19 Page 29 D6-54446 Jun 15/2017 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 156 M81969/8-06 MS27495R20 RX20-3 Burndy 10-296943-20 Bendix M81969/14-02 Plastic White MS27509R20 MS27534-20 11-8675-16 Bendix 11-8795-16 Bendix Metal M81969/8-08 MS27495R16 RX16-9 Burndy M81969/14-03 Plastic White MS27534-16 20-63-19 Page 30 D6-54446 Jun 15/2017 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 157 If the contact does not release: Pull the removal tool out of the contact cavity. Turn the removal tool approximately 90 degrees. Do Step 4.A.(2) through Step 4.A.(5) again. 20-63-19 Page 31 D6-54446 Jun 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...

  • Page 158: Connector Assembly

    M22520/2-01 M22520/2-07 ST2220-10 Boeing ST2220-10-2 Boeing 612916 Buchanan Blue Yellow M22520/1-01 M22520/1-04 WA27F Daniels M22520/1-04 M22520/2-01 M22520/2-10 WA22 Daniels M22520/2-10 ST2220-1-Y Boeing ST2220-1-12 Boeing 20-63-19 Page 32 D6-54446 Jun 15/2019 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 159 M22520/2-10 Amphenol/ MS3191-1 11-7771-31 Bendix ST2220-1-Y Boeing ST2220-1-12 Boeing M22520/1-01 M22520/1-04 Blue WA27F Daniels M22520/1-04 Blue Amphenol/ MS3191-1 11-7771-29 Bendix ST2220-1-Y Boeing ST2220-1-2 Boeing 20-63-19 Page 33 D6-54446 Jun 15/2019 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 160 Boeing ST2220-1-2 Boeing 11148 Buchanan Blue 614019 Buchanan Blue M22520/1-01 M22520/1-04 Blue WA27F Daniels M22520/1-04 Blue Amphenol/ MS3191-1 11-7771-29 Bendix ST2220-1-Y Boeing ST2220-1-2 Boeing 20-63-19 Page 34 D6-54446 Jun 15/2019 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 161 Boeing 11148 Buchanan Yellow 614019 Buchanan Yellow M22520/1-01 M22520/1-04 Yellow WA27F Daniels M22520/1-04 Yellow Amphenol/ MS3191-1 11-7771-43 Bendix ST2220-1-Y Boeing ST2220-1-3 Boeing 1716P-1 Daniels 20-63-19 Page 35 D6-54446 Feb 15/2021 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 162 M22520/2-01 M22520/2-06 ST2220-10 Boeing ST2220-10-1 Boeing 612916 Buchanan Blue Yellow M22520/1-01 M22520/1-04 WA27F Daniels M22520/1-04 M22520/2-01 M22520/2-10 WA22 Daniels M22520/2-10 ST2220-1-Y Boeing ST2220-1-12 Boeing 20-63-19 Page 36 D6-54446 Jun 15/2019 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 163 M22520/2-10 Amphenol/ MS3191-1 11-7771-31 Bendix ST2220-1-Y Boeing ST2220-1-12 Boeing M22520/1-01 M22520/1-04 Blue WA27F Daniels M22520/1-04 Blue Amphenol/ MS3191-1 11-7771-29 Bendix ST2220-1-Y Boeing ST2220-1-2 Boeing 20-63-19 Page 37 D6-54446 Jun 15/2019 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 164 Boeing ST2220-1-2 Boeing 11148 Buchanan Blue 614019 Buchanan Blue M22520/1-01 M22520/1-04 Blue WA27F Daniels M22520/1-04 Blue Amphenol/ MS3191-1 11-7771-29 Bendix ST2220-1-Y Boeing ST2220-1-2 Boeing 20-63-19 Page 38 D6-54446 Jun 15/2019 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 165 Boeing ST2220-1-3 Boeing 11148 Buchanan Yellow 614019 Buchanan Yellow M22520/1-01 M22520/1-04 Yellow WA27F Daniels M22520/1-04 Yellow Amphenol/ MS3191-1 11-7771-43 Bendix ST2220-1-Y Boeing ST2220-1-3 Boeing 20-63-19 Page 39 D6-54446 Jun 15/2019 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 166 M22520/2-01 M22520/2-09 ST2220-10 Boeing ST2220-10-1 Boeing 612916 Buchanan Blue Yellow M22520/1-01 M22520/1-04 WA27F Daniels M22520/1-04 M22520/2-01 M22520/2-10 WA22 Daniels M22520/2-10 Amphenol/ MS3191-1 11-7771-30 Bendix 20-63-19 Page 40 D6-54446 Jun 15/2019 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 167 M22520/2-10 Amphenol/ MS3191-1 11-7771-30 Bendix ST2220-1-Y Boeing ST2220-1-12 Boeing M22520/1-01 M22520/1-04 Blue WA27F Daniels M22520/1-04 Blue Amphenol/ MS3191-1 11-7771-28 Bendix ST2220-1-Y Boeing ST2220-1-2 Boeing 20-63-19 Page 41 D6-54446 Jun 15/2019 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 168 Boeing ST2220-1-2 Boeing 11148 Buchanan Blue 614019 Buchanan Blue M22520/1-01 M22520/1-04 Blue WA27F Daniels M22520/1-04 Blue Amphenol/ MS3191-1 11-7771-28 Bendix ST2220-1-Y Boeing ST2220-1-2 Boeing 20-63-19 Page 42 D6-54446 Jun 15/2019 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 169 Boeing 11148 Buchanan Yellow 614019 Buchanan Yellow M22520/1-01 M22520/1-04 Yellow WA27F Daniels M22520/1-04 Yellow Amphenol/ MS3191-1 11-7771-43 Bendix ST2220-1-Y Boeing ST2220-1-3 Boeing 1716P-1 Daniels 20-63-19 Page 43 D6-54446 Feb 15/2021 ECCN 9E991 BOEING PROPRIETARY - See title page for details...

  • Page 170: Cable Preparation For Shield Termination In The Connector Insert

    • Subject 20-10-15 for the procedure to assemble a shield ground wire. Make sure that the free end of the shield ground wire is pointed forward to the end of the cable. 20-63-19 Page 44 D6-54446 Jun 15/2017 ECCN 9E991 BOEING PROPRIETARY - See title page for details...

  • Page 171: Cable Preparation For Shield Termination - Isolated Shields, Solder Sleeve And Dead End

    Remove the necessary length of the cable jacket from the end of the cable. Refer to: • Table 19 • Figure 33 • Subject 20-00-15. 20-63-19 Page 45 D6-54446 Jun 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 172 0.75 ±0.03 in. (19.05 ±0.76 mm). Refer to: • Figure 35 • Subject 20-00-15 for the cable jacket removal procedures. 20-63-19 Page 46 D6-54446 Jun 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...

  • Page 173: Standard Contact Assembly

    Table 20 INSULATION REMOVAL LENGTH Removal Length L Wire Size Contact (inch) Special Instructions (AWG) Size Maximum Target Minimum 0.17 0.14 0.14 0.17 0.14 0.14 20-63-19 Page 47 D6-54446 Jun 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 174 • Figure 37 • Table 20 for the insulation removal length • Subject 20-00-15 for the insulation removal procedures. 2446140 S00061544325_V1 INSULATION REMOVAL LENGTH Figure 37 20-63-19 Page 48 D6-54446 Feb 15/2021 ECCN 9E991 BOEING PROPRIETARY - See title page for details...

  • Page 175: Assembly Of A Contact With Oversize Wire

    Assembly of a Contact with Oversize Wire This procedure is applicable if the outside diameter of the wire insulation is larger than the maximum wire O.D. specified in Table 21. 20-63-19 Page 49 D6-54446 Jun 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...

  • Page 176: Necessary Materials

    Remove 1.50 ±0.06 in. (38.10 ±1.52 mm) length of insulation from the end of the wire. Refer to Figure 39. 2448348 S00061547172_V1 INSULATION REMOVAL LENGTH Figure 39 Put the sleeve on the wire. 20-63-19 Page 50 D6-54446 Oct 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 177 Refer to Figure 41. 2448362 S00061547174_V1 POSITION OF THE INNER HEAT SHRINKABLE SLEEVE Figure 41 Shrink the sleeve into its position. Refer to Subject 20-10-14. 20-63-19 Page 51 D6-54446 Jun 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 178 Part Number Setting Suppler Part Number Supplier M22520/2-01 M22520/2-31 Table 24 FERRULE CRIMP TOOLS Basic Unit Part Number Supplier Part Number Supplier M22520/5-01 M22520/5-05 20-63-19 Page 52 D6-54446 Jun 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...

  • Page 179: Necessary Tools

    Remove 0.75 ±0.03 in. (19.05 ±0.76 mm) of the cable jacket from the end of the coax cable. Refer to Figure 43. Use the ferrule to prepare the shield: 20-63-19 Page 53 D6-54446 Jun 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 180 Make sure that you do not cut the round shield strands. Use the retainer to prepare the dielectric: Put the nut on the retainer. Refer to Figure 45. 20-63-19 Page 54 D6-54446 Jun 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 181 Put the center conductor into the center contact crimp barrel. Make a selection of a Center Contact Crimp Tool and Locator from Table 23. Crimp the center contact. Refer to Figure 47. 20-63-19 Page 55 D6-54446 Jun 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 182 Refer to Figure 49. 2449291 S00061547182_V1 THE FERRULE ON THE SHIELD Figure 49 Make a selection of a Ferrule Crimp Tool from Table 24. 20-63-19 Page 56 D6-54446 Jun 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 183 Hold the center contact crimp area and, at the same time, push the push tool until the rear insulator is between the shoulder of the center contact and the retainer. Refer to Figure 52. 20-63-19 Page 57 D6-54446 Jun 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 184 Put the front insulator, large end first, on the center contact. (20) Push the front insulator rearward until the front insulator is against the shoulder of the center contact. Refer to Figure 53. 20-63-19 Page 58 D6-54446 Jun 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 185 Make sure that the distance between the nut and the outer contact body is 0.035 in. (0.889 mm) maximum. Refer to Figure 53. (25) Push the seal boot against the contact assembly until it stops. 20-63-19 Page 59 D6-54446 Oct 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...

  • Page 186: Assembly Of Size 8 Bacc47Gm1 And Bacc47Gn1 Quadrax Contacts

    Make a selection of an outer contact crimp tool from Table 28. Cut the cable perpendicular to its longitudinal axis. Put the seal boot on the cable. Refer to Figure 54. 20-63-19 Page 60 D6-54446 Jun 15/2017 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 187 Move the seal boot away from the end of the cable. Remove 0.53 ±0.02 in. (13.46 ±0.51 mm) of the outer jacket from the end of the cable. Refer to Figure 55. 20-63-19 Page 61 D6-54446 Jun 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 188 Push the ferrule rearward until it is against the end of the outer jacket. Refer to Figure 56. Fold the outer round shield back on the ferrule. Refer to Figure 57. 20-63-19 Page 62 D6-54446 Jun 15/2017 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 189 Remove 0.14 ±0.02 in. (3.56 ±0.51 mm) of insulation from the end of each of the four colored wires. Refer to: • Figure 57 20-63-19 Page 63 D6-54446 Jun 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 190 Only one of these configurations is possible at each end of the quadrax cable. 2448178 S00061547191_V1 INSTALLATION OF THE INNER CONTACTS IN THE SPACER CHANNELS Figure 58 20-63-19 Page 64 D6-54446 Jun 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 191 SATISFACTORY POSITIONS OF THE COLORED WIRES IN THE SPACER - KEYWAY BETWEEN THE RED AND YELLOW WIRES Figure 59 2449061 S00061547193_V1 SATISFACTORY POSITIONS OF THE COLORED WIRES IN THE BACC47GN SOCKET SPACER Figure 60 20-63-19 Page 65 D6-54446 Jun 15/2017 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 192 Figure 61 (17) Align the insulator and the spacer. Refer to Figure 62. Make sure that the insulator keyway and the spacer keyway are aligned. 20-63-19 Page 66 D6-54446 Jun 15/2017 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 193 Align the key of the outer contact and the keyways of the insulator and the spacer. Refer to Figure (20) Push the insulator assembly into the outer contact until it stops. Refer to Figure 64. Make sure that: 20-63-19 Page 67 D6-54446 Jun 15/2017 ECCN 9E991 BOEING PROPRIETARY - See title page for details...

  • Page 194: Contact Insertion

    Remove all of the strands of the shield that extend beyond the rear edge of the outer contact. Contact Insertion Table 29 CONTACT INSERTION TOOLS Insertion Tool Contact Size Material Part Number Supplier Color Metal DAK225-22 Daniels Plastic M81969/16-04 Green 20-63-19 Page 68 D6-54446 Jun 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 195 Brown MS27495A22 RTM22-1 Burndy 10-296940-22 Bendix Plastic Brown MS27509A22 11-8674-20 Bendix 11-8794-20 Bendix Metal M81969/8-05 MS27495A20 RTM20-17 Burndy 10-296940-20 Bendix M81969/14-02 Plastic MS27509A20 MS27534-20 20-63-19 Page 69 D6-54446 Jun 15/2017 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 196 Lubricate the rear grommet of the connector with isopropyl alcohol. Put the contact assembly in the insertion tool. Axially align the insertion tool and the contact cavity at the rear of the connector. 20-63-19 Page 70 D6-54446 Jun 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...

  • Page 197: Installation Of Size 8 Quadrax Contacts

    Refer to: • Figure 66 for the polarization key of the quadrax contact • Figure 67 for the keyway of the quadrax contact cavity. 20-63-19 Page 71 D6-54446 Jun 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 198 2448169 S00061547201_V1 POLARIZATION KEY OF THE QUADRAX CONTACT Figure 66 2448183 S00061547202_V1 QUADRAX CONTACT CAVITY KEYWAY - REAR FACE OF THE CONNECTOR Figure 67 20-63-19 Page 72 D6-54446 Jun 15/2017 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 199 DO NOT PULL THE WIRE WITH A STRONG OR A SUDDEN FORCE. THE FORCE CAN CAUSE DAMAGE TO THE CONNECTOR OR THE CONTACT. CAUTION 20-63-19 Page 73 D6-54446 Jun 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...

  • Page 200: Spare Contact And Seal Plug Installation

    PLUG AND RECEPTACLE CONNECTION Connection of the Plug and the Receptacle Refer to Subject 20-60-06 for the procedure for the connection of the plug and the receptacle. 20-63-19 Page 74 D6-54446 Jun 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 201 Cable Preparation - Shield Pull Through Shield Termination Backshell Assembly Assembly of the Shield Termination Ring Shield Sock Termination Installation of the Strain Relief Boot 20-63-20 Page 1 D6-54446 Jun 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 202 BACC63EB CONNECTOR PART NUMBER STRUCTURE Figure 1 Contact Part Numbers 2449031 S00061547206_V1 BACC47GC CONTACT Figure 2 2446651 S00061545900_V1 EXAMPLE OF A CONTACT SIZE Figure 3 20-63-20 Page 2 D6-54446 Oct 15/2015 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 203 45 Degree Boot Wiring Assembly Components Table 3 WIRING ASSEMBLY COMPONENTS Component Type Specification PTFE A-A-59474 Tape Silicone, Type I A-A-59163 Silicone, Type II A-A-59163 20-63-20 Page 3 D6-54446 Jun 15/2021 ECCN 9E991 BOEING PROPRIETARY - See title page for details...

  • Page 204: Necessary Tools

    AND UNSATISFACTORY PERFORMANCE OF THE BACKSHELL. 2448412 S00061545211_V1 BACKSHELL HEX NUT TOOL Figure 4 Table 4 HEX COUPLING NUT TOOLS Tool Shell Size Part Number Supplier 600-091-08 Glenair 20-63-20 Page 4 D6-54446 Jun 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...

  • Page 205: Connector Disassembly

    Make a selection of needle nose pliers. NOTE: The removal of a seal plug with the hand is a satisfactory alternative to the removal with the pliers. 20-63-20 Page 5 D6-54446 Jun 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...

  • Page 206: Accessory Adapter Removal

    Figure 5 BACKSHELL DISASSEMBLY Separation of the Backshell from the Connector 2449169 S00061547209_V1 BACKSHELL WITH STRAIN RELIEF BOOT Figure 6 Refer to Figure 6. 20-63-20 Page 6 D6-54446 Jun 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 207 Hold the connector with the connector adapter, and at the same time, loosen the backshell with the hex coupling nut holding tool. Disengage the backshell from the connector. (11) Push the backshell rearward on the wire harness. 20-63-20 Page 7 D6-54446 Jun 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...

  • Page 208: Shield Termination Ring Removal

    Remove the necessary length of insulation from the end of the wire. Refer to: • Table 10 • Figure 7 • Subject 20-00-15 for the procedure to remove the insulation. 20-63-20 Page 8 D6-54446 Oct 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...

  • Page 209: Contact Insertion

    • The tool is not broken • The tool tip does not have a bend • The tool tip does not have burrs, nicks, or sharp edges. 20-63-20 Page 9 D6-54446 Jun 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 210 Refer to Table 13. 2448977 S00061547212_V1 CONTACT INSERTION TOOL Figure 8 Align the contact assembly and the contact cavity. Refer to Figure 9. 20-63-20 Page 10 D6-54446 Jun 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 211 Carefully push the contact assembly into the contact cavity until it stops. Refer to Figure 10. Make sure that the contact assembly and the contact cavity stay aligned. 20-63-20 Page 11 D6-54446 Jun 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 212 If the contact is not locked in the contact cavity: Remove the contact assembly from the contact cavity. Do Step 5.B.(3) through Step 5.B.(7) again. 20-63-20 Page 12 D6-54446 Oct 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...

  • Page 213: Seal Plug Installation

    LENGTH OF THE SHIELD SOCK FOR A STRAIN RELIEF BOOT BACKSHELL Figure 12 Put the wire harness in the shield sock. Refer to Figure 13. 20-63-20 Page 13 D6-54446 Jun 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 214 Put the adapter assembly on the wire harness. Refer to Figure 14. 2448931 S00061547216_V1 POSITION OF THE ACCESSORY ADAPTER ON THE CABLE Figure 14 20-63-20 Page 14 D6-54446 Jun 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...

  • Page 215: Cable Preparation - Shield Pull Through Shield Termination

    SHIELD PULL THROUGH SHIELD GROUND WIRE - STANDARD CONFIGURATION Figure 16 Remove the necessary length from the end of the wires. Refer to Figure 16. 20-63-20 Page 15 D6-54446 Oct 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...

  • Page 216: Backshell Assembly

    Align the backshell tab and the master key or keyway of the connector. Refer to Figure 18. 20-63-20 Page 16 D6-54446 Oct 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 217 Examine the teeth of the backshell and the connector through the inspection hole. Refer to Figure Make sure that the backshell teeth are fully engaged with the connector teeth. 20-63-20 Page 17 D6-54446 Jun 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 218 THE INITIAL SETTING. TOO MUCH TORQUE CAN RESET THE INITIAL SETTING WHICH CAN CAUSE AN INCORRECT TORQUE INDICATION. CAUTION Do Step 6.C.(15)(a) and Step 6.C.(15)(b) again until the specified torque is applied. 20-63-20 Page 18 D6-54446 Oct 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...

  • Page 219: Assembly Of The Shield Termination Ring

    If the tape does not prevent the movement of the shield termination ring, wind more layers of the tape on the harness. Make sure that: 20-63-20 Page 19 D6-54446 Jun 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 220 • The end of the shield ground wire does not extend farther than 0.2 in. (5.08 mm) from the rear end of the tape • The shield ground wires are not loose. 20-63-20 Page 20 D6-54446 Oct 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...

  • Page 221: Shield Sock Termination

    • The tape extends 0.50 ±0.25 in. (12.70 ±6.35 mm) farther than the end of the fold of the shield sock • The end of the shield sock has tape on it 20-63-20 Page 21 D6-54446 Oct 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...

  • Page 222: Installation Of The Strain Relief Boot

    Put the Master Key or Keyway of the connector in the specified clock position. Refer to Figure 24. NOTE: If the clock position is not specified, put the Master Key or Keyway in clock position 12. 20-63-20 Page 22 D6-54446 Oct 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 223 Figure 25. NOTE: The boot can be turned manually around the backshell and the wire harness. 20-63-20 Page 23 D6-54446 Oct 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 224 • Stops 1.1 ±0.1 in. (27.94 ±2.54 mm) farther than the end of the shield sock • Has an approximately 50% overlap • Has an approximately 100% overlap at the end. 20-63-20 Page 24 D6-54446 Oct 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 225 0.75 in. (19.05 mm) overlap with the rear end of the tape. Shrink the sleeve into its position. Refer to: • Figure 27 • Subject 20-10-14 for the procedure to install the sleeve. 20-63-20 Page 25 D6-54446 Oct 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 226 707, 727-787 STANDARD WIRING PRACTICES MANUAL ASSEMBLY OF BACC63EB CONNECTORS 2449168 S00061547229_V1 POSITION OF THE HEAT SHRINKABLE SLEEVE Figure 27 20-63-20 Page 26 D6-54446 Jun 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 227 Contact Insertion Seal of an Empty Contact Cavity Backshell and Strain Relief Assembly APPROVED TOOL SUPPLIERS Contact Removal Tools Contact Crimp Tools Contact Insertion Tools 20-63-21 Page 1 D6-54446 Oct 15/2017 ECCN 9E991 BOEING PROPRIETARY - See title page for details...

  • Page 228: General Data

    PART NUMBERS AND DESCRIPTION Connector Part Numbers Table 2 CONNECTOR PART NUMBERS Part Number Supplier Reference MS3470() Figure 1 MS3475() Figure 1 MS3476() Figure 1 20-63-21 Page 2 D6-54446 Oct 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 229 MIL-C-26482 SERIES II CONNECTOR PART NUMBER STRUCTURE Figure 1 Contact Part Numbers 2448999 S00061545899_V1 LOCATION OF THE COLOR BANDS ON THE M39029/4 AND /5 REAR RELEASE CONTACTS Figure 2 20-63-21 Page 3 D6-54446 Oct 15/2015 ECCN 9E991 BOEING PROPRIETARY - See title page for details...

  • Page 230: Contact Part Numbers

    Part Number Supplier Engaging Crimp Barrel Band Color Brown M39029/4-110 Brown Black Brown M39029/4-20-20 Brown Black Brown M39029/5-115 Brown Green Socket Brown M39029/5-20-20 Brown Green 20-63-21 Page 4 D6-54446 Feb 15/2016 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 231 ALTERNATIVE CONTACT PART NUMBERS Specified Contact Alternative Contact Part Number Supplier Part Number Supplier M39029/4-12-12 M39029/4-113 M39029/4-16-16 M39029/4-111 M39029/4-20-20 M39029/4-110 M39029/5-12-12 M39029/5-118 M39029/5-16-16 M39029/5-116 20-63-21 Page 5 D6-54446 Feb 15/2016 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 232 14-12 Figure 7 14-15 Figure 7 14-18 Figure 7 14-19 Figure 7 16-8 Figure 8 16-23 Figure 8 16-26 Figure 8 16A99 Figure 8 20-63-21 Page 6 D6-54446 Oct 15/2015 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 233 NOTE: Figure 4 through Figure 12 show the front face of an insert that has pins. The view of the front face of an insert that has sockets is the mirror image of this view. 20-63-21 Page 7 D6-54446 Oct 15/2015 ECCN 9E991 BOEING PROPRIETARY - See title page for details...

  • Page 234: Insert Configurations

    ASSEMBLY OF MIL-C-26482 SERIES II REAR RELEASE CONNECTORS 2446131 S00061546576_V1 8-() INSERT CONFIGURATIONS Figure 4 2446132 S00061546577_V1 10-() INSERT CONFIGURATIONS Figure 5 2446133 S00061546578_V1 12-() INSERT CONFIGURATIONS Figure 6 20-63-21 Page 8 D6-54446 Oct 15/2015 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 235 STANDARD WIRING PRACTICES MANUAL ASSEMBLY OF MIL-C-26482 SERIES II REAR RELEASE CONNECTORS 2446134 S00061546579_V1 14-() INSERT CONFIGURATIONS Figure 7 2446135 S00061546580_V1 16-() INSERT CONFIGURATIONS Figure 8 20-63-21 Page 9 D6-54446 Oct 15/2015 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 236 STANDARD WIRING PRACTICES MANUAL ASSEMBLY OF MIL-C-26482 SERIES II REAR RELEASE CONNECTORS 2446136 S00061546581_V1 18-() INSERT CONFIGURATIONS Figure 9 2446137 S00061546582_V1 20-() INSERT CONFIGURATIONS Figure 10 20-63-21 Page 10 D6-54446 Oct 15/2015 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 237 STANDARD WIRING PRACTICES MANUAL ASSEMBLY OF MIL-C-26482 SERIES II REAR RELEASE CONNECTORS 2446138 S00061546583_V1 22-() INSERT CONFIGURATIONS Figure 11 2446139 S00061546584_V1 24-() INSERT CONFIGURATIONS Figure 12 20-63-21 Page 11 D6-54446 Oct 15/2015 ECCN 9E991 BOEING PROPRIETARY - See title page for details...

  • Page 238: Connector Disassembly

    M83723/31-16 White MS27534-16 White NAS1664-16 White M81969/14-04 White M83723/31-12 White MS27534-12 White NAS1664-12 White Make a selection of a removal tool from Table 7. 20-63-21 Page 12 D6-54446 Jun 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...

  • Page 239: Unwired Contact Removal

    Make a selection of a contact removal tool from Table 8. Remove the seal plug from the contact cavity. Axially align the tool and the contact cavity at the rear of the connector. 20-63-21 Page 13 D6-54446 Jun 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...

  • Page 240: Connector Assembly

    Remove the necessary length of insulation from the end of the wire. Refer to: • Figure 13 • Table 9 for the insulation removal length • Subject 20-00-15 for the insulation removal procedure. 20-63-21 Page 14 D6-54446 Jun 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 241 • The conductor can be seen in the inspection hole • The distance from the end of the insulation to the crimp barrel is not more that 0.03 in. (0.76 mm). 20-63-21 Page 15 D6-54446 Oct 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 242 Color CIET20-1 M81969/14-02 M83723/31-20 MS27534-20 NAS1664-20 CIET16-3 Blue M81969/14-03 Blue M83723/31-16 Blue MS27534-16 Blue NAS1664-16 Blue M81969/14-04 Yellow M83723/31-12 Yellow MS27534-12 Yellow NAS1664-12 Yellow 20-63-21 Page 16 D6-54446 Oct 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...

  • Page 243: Seal Of An Empty Contact Cavity

    Do Step 5.C.(2) through Step 5.C.(6) again. Seal of an Empty Contact Cavity All empty contact cavities must be sealed. Refer to Subject 20-60-08. 20-63-21 Page 17 D6-54446 Jun 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...

  • Page 244: Backshell And Strain Relief Assembly

    M83723/31-16 M83723/31-20 MS27534-12 MS27534-16 MS27534-20 NAS1664-12 NAS1664-16 NAS1664-20 Contact Crimp Tools Table 13 CONTACT CRIMP TOOL SUPPLIERS Crimp Tool Supplier M22520/1-01 M22520/1-02 M22520/2-01 M22520/2-02 20-63-21 Page 18 D6-54446 Oct 15/2017 ECCN 9E991 BOEING PROPRIETARY - See title page for details...

  • Page 245: Contact Insertion Tools

    CONTACT INSERTION TOOL SUPPLIERS Insertion Tool Supplier CIET16-3 ITT Cannon CIET20-1 ITT Cannon M81969/14-02 M81969/14-03 M81969/14-04 M83723/31-12 M83723/31-16 M83723/31-20 MS27534-12 MS27534-16 MS27534-20 NAS1664-12 NAS1664-16 NAS1664-20 20-63-21 Page 19 D6-54446 Oct 15/2017 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 247 Connector Separation Contact Removal CONNECTOR ASSEMBLY Contact Assembly Contact Insertion CONNECTOR INSTALLATION Plug and Receptacle Connection APPROVED TOOL SUPPLIERS Crimp Tools Insertion and Removal Tools 20-63-22 Page 1 D6-54446 Jun 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...

  • Page 248: Part Numbers And Description

    Part Number Supplier Part Number Supplier CSLT2-21P() Cory Components CSLT2-21P() Tri-Star Contact Part Numbers 2449045 S00061547234_V1 LOCATION OF THE CONTACT COLOR BANDS Figure 1 20-63-22 Page 2 D6-54446 Oct 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...

  • Page 249: Contact Part Numbers

    Supplier Part Number Supplier CB005-5P Cory Components CB005-5P Tri-Star Insert Configurations Table 5 INSERT CONFIGURATIONS Contact Cavity Insert Configuration Reference Count Size Figure 3 20-63-22 Page 3 D6-54446 Feb 15/2016 ECCN 9E991 BOEING PROPRIETARY - See title page for details...

  • Page 250: Connector Disassembly

    Make a selection of a screwdriver. Turn the screw counterclockwise to align the slots on the screw head with the red indicator lines. Refer to Figure 4. 20-63-22 Page 4 D6-54446 Oct 15/2015 ECCN 9E991 BOEING PROPRIETARY - See title page for details...

  • Page 251: Contact Removal

    DO NOT USE MORE THAN THE NECESSARY AMOUNT OF FORCE TO PUSH THE TOOL INTO THE CONTACT CAVITY. DAMAGE TO THE CONTACT RETENTION CLIPS CAN OCCUR. CAUTION 20-63-22 Page 5 D6-54446 Jun 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...

  • Page 252: Connector Assembly

    Removal Length L Wire Size (inch) Crimp Barrel Size Special Instructions (AWG) Target Tolerance 0.40 ±0.03 Fold back conductor 0.20 ±0.03 0.20 ±0.03 0.20 ±0.03 20-63-22 Page 6 D6-54446 Jun 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 253 KAP13-1 K13-1 WA22LC M22520/2-08 K13-1 AFM 8 M22520/2-08 K13-1 M22520/2-01 M22520/2-08 MS3191-1 P20-3191-1 11697-1 ST2220-1-Y ST2220-1-43 K13-1 WA22 M22520/2-08 WA22AP KAP13-1 K13-1 WA22LC M22520/2-08 20-63-22 Page 7 D6-54446 Oct 15/2017 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 254 Refer to Figure 6. Make sure that: • All the strands of the conductor are in the crimp barrel 20-63-22 Page 8 D6-54446 Oct 15/2015 ECCN 9E991 BOEING PROPRIETARY - See title page for details...

  • Page 255: Contact Insertion

    Axially align the insertion tool and the contact cavity at the rear of the connector. Carefully push the contact assembly into the contact cavity until it stops. 20-63-22 Page 9 D6-54446 Jun 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...

  • Page 256: Connector Installation

    From the rear of the plug, turn the locking screw clockwise until the slot in the screw are aligned with the green indicator lines. Refer to Figure 7. 20-63-22 Page 10 D6-54446 Jun 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...

  • Page 257: Approved Tool Suppliers

    11697-1 Buchanan AFM 8 Daniels K13-1 Daniels K250 Daniels Daniels KAP13-1 Daniels M22520/2-01 M22520/2-06 MS3191-1 P20-3191-1 ITT Cannon ST2220-1-43 Boeing ST2220-1-Y Boeing WA22 Daniels 20-63-22 Page 11 D6-54446 Jun 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...

  • Page 258: Insertion And Removal Tools

    Crimp Tool Supplier WA22AP Daniels WA22LC Daniels Insertion and Removal Tools Table 11 INSERTION AND REMOVAL TOOL SUPPLIERS Tool Supplier DAK145 Daniels DRK145 Daniels M81969/1-02 20-63-22 Page 12 D6-54446 Jun 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 259 Contact Part Numbers and Components CONNECTOR DISASSEMBLY Contact Removal Removal Seal Rod CONNECTOR ASSEMBLY Contact Assembly Contact Insertion Seal Rod Installation Protective Cap Installation PLUG AND RECEPTACLE CONNECTION 20-63-23 Page 1 D6-54446 Oct 15/2017 ECCN 9E991 BOEING PROPRIETARY - See title page for details...

  • Page 260: Part Numbers And Description

    Make a selection of a contact removal tool from Table 4. At the rear of the connector, put the removal tool on the wire. Axially align the removal tool and the contact cavity. 20-63-23 Page 2 D6-54446 Oct 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...

  • Page 261: Removal Seal Rod

    TT-I-735 An available source Contact Assembly Table 6 Insulation Removal Length Removal Length (inch) Wire Size (AWG) Crimp Barrel Size Target Tolerance 0.36 ±0.02 20-63-23 Page 3 D6-54446 Jun 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...
  • Page 262 Put the end of the conductor in the crimp barrel of the contact. Refer to Figure 3. Make sure that: All the conductor strands are in the crimp barrel. 20-63-23 Page 4 D6-54446 Oct 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...

  • Page 263: Contact Insertion

    Make sure that the rear end of the seal boot is not farther than 1.9 in. (48.26 mm) from the forward end of the connector. 20-63-23 Page 5 D6-54446 Oct 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...

  • Page 264: Seal Rod Installation

    Engage the threads of the jam nut and the installation threads of the receptacle. Install a dust cap on the connector. Refer to \Subject 20-10-11. PLUG AND RECEPTACLE CONNECTION 20-63-23 Page 6 D6-54446 Jun 15/2023 ECCN 9E991 BOEING PROPRIETARY - See title page for details...

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