What was found
AT C-CHECK, FUSELAGE SKIN GOUGED BELOW NR 1 ENGINE STRUT FWD END. BURNISHED SKIN, OUT OF LIMITS. CUT OUT DAMAGED AREA 1.5 BY .75. INSTALLED REPAIR PER SRM 53-30-3.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AT C-CHECK, FUSELAGE SKIN GOUGED BELOW NR 1 ENGINE STRUT FWD END. BURNISHED SKIN, OUT OF LIMITS. CUT OUT DAMAGED AREA 1.5 BY .75. INSTALLED REPAIR PER SRM 53-30-3.