ARMY TM 10-1670-282-23&P
AIR FORCE T.O. 13CS-3G-2
NAVY NAVAIR 13-1-33
(7)
On the upper and lower ends of the cloth material, make a 1/2-inch tumunder. Insure the folded edge of the upper
end is a lined with the upper edge of the vent reinforcement (upper lateral band) or lower annular ring
reinforcement, as applicable.
(8)
A
line the folded edge of the lower end with the lower edge of the upper annular ring reinforcement or skirt
reinforcement (lower lateral band), as applicable.
(9)
Temporarily secure the turnunders by basting in accordance with para. 2-17. Remove the pushpins used in 1
above.
(10)
Begin securing the replacement panel by stitching a single row, 1/8 Inch, along the outer edge of all the panel
folded edges. Stitching will be made using the specifics in table 2-3.
(11)
Reinvert the canopy to the outside and trim the raw edges of the panel material along the inside edge of each seam
surrounding the replacement panel.
(12)
Complete the panel installation by stitching a second single row along the Inside of the panel folded edges, 1/8
Inch out from the inside edge of each radial tape, the vent or skirt reinforcement (upper or lower lateral band), as
applicable, and the applicable annular ring reinforcement. Stitching will be made using the specifics in table 2-3.
2-73
