What was found
FUSELAGE SKIN GOUGED AT PREVIOUS BLEND. REMOVED DAMAGED AREA. INSTALLED REPAIR PARTS PER SRM 53-04.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE SKIN GOUGED AT PREVIOUS BLEND. REMOVED DAMAGED AREA. INSTALLED REPAIR PARTS PER SRM 53-04.