ARMY TM 10-1670-282-23&P
AIR FORCE T.O. 13C5-30-2
NAVY NAVAIR 13-1-33
2-38.
Panels and Flaps (cont).
(d) Make a 1/2-inch foldback on each raw edge. Pin and baste each foldback to complete prepared hole.
Basting will be performed using procedures in paragraph 2-17a.
(e) Using duck cloth, mark and cut a patch 2-1/2 inches wider and longer than Inside measurements of the
prepared hole.
(f)
Center patch material over prepared hole and pin patch material in position.
(g) Make a 1/2-in,h foldunder on each edge of patch material and baste patch to prepared area. Basting will
be performed using procedures in paragraph 2-17.
(h) Remove pushpins securing the hem to repair table and secure the patch by stitching, using applicable
details in figure 2-64 and stitch with a light-duty sewing machine, size E nylon thread, 7 to 11 stitches per
inch. Make first row of stitching completely around patch. Turn pack Inside out and make a second row
of stitching around prepared hole. Stitching will be performed in accordance with paragraph 2-17b.
(4)
Restenciling. As required, restencil identification markings on the suspension line protector flap using
procedures in paragraph 2-19.
Figure 2-64. Patching Pack Panels and Flaps.
2-104
