What was found
RIGHT AFT VERTICAL STAB TO FUSELAGE SEAL PANEL AREA FUSELAGE SKIN WORN. REPAIRED IAW SRM 53-00-01 FIG 201 REPAIR ONE REV 91.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
RIGHT AFT VERTICAL STAB TO FUSELAGE SEAL PANEL AREA FUSELAGE SKIN WORN. REPAIRED IAW SRM 53-00-01 FIG 201 REPAIR ONE REV 91.