What was found
DURING OP 16 MAINT CHECK, FOUND FUSELAGE SKIN WORN AT LONGERON 26L, STA 815, UNDER FUSELAGE FAIRING. TRIMMED DAMAGED AREA WHICH IS FOR A LAP SEAM. INSTALLED REPAIR PER SRM 53-04 FIG 12B.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING OP 16 MAINT CHECK, FOUND FUSELAGE SKIN WORN AT LONGERON 26L, STA 815, UNDER FUSELAGE FAIRING. TRIMMED DAMAGED AREA WHICH IS FOR A LAP SEAM. INSTALLED REPAIR PER SRM 53-04 FIG 12B.