What was found
RIGHT FORWARD FUSELAGE SKIN HAS 2" CREASE BETWEEN LONGERON 25 & LONGERON 26 AT APPROXIMATELY F/S 141. CUT OUT DAMAGE IAW SRM53-04 FIG 38, SHEET 34. INSTALLED REPAIR PARTS IAW SRM 53-04 FIG 38, SHEET 34.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
RIGHT FORWARD FUSELAGE SKIN HAS 2" CREASE BETWEEN LONGERON 25 & LONGERON 26 AT APPROXIMATELY F/S 141. CUT OUT DAMAGE IAW SRM53-04 FIG 38, SHEET 34. INSTALLED REPAIR PARTS IAW SRM 53-04 FIG 38, SHEET 34.