What was found
LOWER FUSELAGE SKIN HAS HOLE AT STA 380, BL 0. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. INSTALLED SKIN REPAIR PER SRM 53-00-01, FIG 214, AND SRM 51-40-2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LOWER FUSELAGE SKIN HAS HOLE AT STA 380, BL 0. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. INSTALLED SKIN REPAIR PER SRM 53-00-01, FIG 214, AND SRM 51-40-2.