As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
EXTERIOR FUSELAGE SKIN RT SIDE AT BS 950E 1 INCH STR S-18R 4 INCH SKIN IS GOUGED. REMOVED DAMAGE REF SRM 53-30-1. NDT'D ORIGINAL MATERIAL THICKNESS .140. REMOVED .044 .096 MATERIAL REMAINING. REPAIRED ON N00256. THIS IS CLASSIFIED AS A MAJOR REPAIR. MATERIAL LOSS OUT OF LIMITS REF SRM 53-30-1 AREA TO BE REPAIRED ON N00256.