As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
WHILE PERFORMING THE TRIM OUT OF THE UPPER SKIN PANEL AT WS 711.50 ON LT AND RT WING FOUND THAT THE TRIM LINE NEEDS TO DEVIATE FROM THE ORIGINAL STRAIGHT TRIM LINE IAW APB DWG 757-3500 TO ALLOW EDGE DISTANCE ON EXISTING FASTERNERS BE MAINTAINED COMMON TO THE FWD SPAR AS SHOWN IN FIG 1. ACCOMPLHISHED ER/A 480619-14 REV ORIGINAL AT REF NON ROUTINE 159723. (DL757101364).