What was found
INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND .75 INCH CRACK, STA 616, LT FRAME INBOARD CHORD, FIRST FASTENER ABOVE CENTER WING SKIN. INSTALLED FILLER AND ANGLE, WEIGHT CHANGE LESS THAN 1 POUND. REPAIRED PER EA 40391. (X)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND .75 INCH CRACK, STA 616, LT FRAME INBOARD CHORD, FIRST FASTENER ABOVE CENTER WING SKIN. INSTALLED FILLER AND ANGLE, WEIGHT CHANGE LESS THAN 1 POUND. REPAIRED PER EA 40391. (X)