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Figure 2-39.  Gore Panel Replacement Details
Figure 2-40.  Radial Tape Restitching Details.

TM-10-1670-279-23P Parachute Cargo Type: 22-Foot Diameter Cargo Extraction Parachute NSN 1670-01-063-3716 and NSN 1670-00-687-5408 Manual
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ARMY TM 10-1670-279-23&P AIR FORCE T.O.  13C5-27-2 NAVY NAVAIR 13-1-28 2-27. Radial Tape. This task covers: Repair Tools: Personnel Required: Knife,  Item 4,  Appendix B 43E(10) Parachute Rigger Knife,  Hot Metal,  Item 5,  Appendix B Sewing Machine,  Zig-Zag,  Item 17,                      Equipment Condition: Appendix B Sewing Machine Light Duty,  Item 16, Cleaned,  paragraph 2-12 Appendix B Inspected,  paragraphs 2-9,  2-13 Shears,  Item 14,  Appendix B Unpacked,  laid flat Pushpins Yardstick,  Item 24,  Appendix B Reference: Materials/Parts: Group No.  01,  MAC,  Section II, Appendix B Thread,  Nylon,  Size E,  Item 26/27 Appendix D Webbing,  Nylon,  Type IV,  1-Inch,  Item 36, Appendix D a. Restitching.   Restitch  radial  tape;  using  a  light  duty  sewing  machine  and  size  E  nylon  thread  of  contrasting color.  Stitch over original pattern,  7 to 11 stitches per inch.  Lock each row of stitches two inches at each end.  When radial  tape  stitching  has  failed  and  section  separation  from  radial  tape  has  occurred  at  the  leading  or  trailing  edge  of ringslots,  the repair will be accomplished as follows: (1) Restitch failure in accordance with original construction.  Sew a double throw zig-zag stitching across the width of radial tape at leading/trailing edge of ringslot.  Zig-zag stitching should be centered on width of reinforced hem of leading/trailing edge and will be stitched in accordance with para.  2-18d (A,  figure 2-40). (2) As an option,  if a zig-zag sewing machine is not available,  a box stitch pattern (double row stitching at box   ends)   1   1/4   inches   in   length   may   be   used.      Box   should   start   on   reinforced   hem   of   leading/trailing   edge, approximately 1/8 inches from edge of ring,  and proceed In length along radial seam of ring (B,  figure 2-40). 2-74







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