If you continue down from where you got this.
The 15th F-86H-1-NH was fitted with the "6-3" wing of the later F-86F, with extended wing tips and wing fences. Wing span was increased from 37.12 feet to 39.1 feet and wing area rose to 313.4 square feet.
In the meantime, on June 11, 1953 the USAF approved an additional contract (NA-203) for 300 F-86H-10-NHs. These differed from earlier F-86Hs primarily in having different electronic equipment and in having the J73-GE-3E engine. The first aircraft was delivered in January of 1955, and the last aircraft on the order was delivered in April of 1956. The last ten H-10s used the so-called "F-40" wing, with extended wingtips and slats on the extended leading edge, which improved low-speed handling. Eventually, all of the remaining Hs in the USAF and ANG inventories were retrofitted with the "F-40" wing.
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