The wing leading edge extension seems to have been enlarged and straightened. The pattern of openings behind the cockpit has also changed.
The division between flap and aileron have been moved further outboard, so the aileron is now noticeably smaller. I wonder if this is done to reduce landing speed or shorten takeoff run by increasing the area of the flap? Or perhaps it was done to move the division between flap and aileron to where the wing folding hing would be in a future carrier version?
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