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Figure 2-41.  Radial Tape Splice Details.
Figure 2-42.  Panel Edge Reinforcement Splicing 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 2-28. Panel Edge Reinforcement. 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,  Light Duty,  Item 16                 Equipment Condition: Appendix B Shears,  Item 14,  Appendix B Cleaned,  paragraph 2-12 Yardstick,  Item 24,  Appendix B Inspected,  paragraphs 2-9,  2-13 Canopy laid flat on repair table Materials/Parts: Reference: Thread,  Nylon Size E,  Item 26127, Appendix D Group No.  01,  MAC,  Section II, Tape,  Nylon,  Type III,  112-inch,  Item 22, Appendix B Appendix D a. Restitching.  Restitching of panel edge reinforcement is authorized.  Use a light duty sewing machine and size E,  nylon thread of contrasting color.  Stitch over the original stitch pattern,  7 to 11 stitches per inch.  Lock each row of stitches two inches at each end.  Stitch according to paragraph 2- 18 and table 2-3. NOTE The panel edges may be spliced only once and will not be replaced. b. Splicing.  A panel edge reinforcement may be spliced one time as follows. (1) Cut a length of 1/2-inch wide,  type III nylon tape long enough to extend 6 inches beyond each side of damaged area and sear ends (para.  2-19). (2) Center webbing length over damaged area and secure splice by stitching a box-stitch formation,  1/16- inch  in  from  each  edge,    full  length  of  splice  material  (figure  2-42).  Use  a  light-duty  sewing  machine, size E nylon thread,  7 to 11 stitches per inch. 2-77







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