What was found
CORROSION ON FRAME IN STA. FS=847 +48 BETWEEN STRINGER 26LH TO 26 RH AT INTERNAL FUSELAGE. FRAME IN STA. FS=847 +48 BETWEEN STRINGER 26LH TO 26 RH AT INTERNAL FUSELAGE WAS REPAIRED PER E.A 81-2021-010 REV. IR
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CORROSION ON FRAME IN STA. FS=847 +48 BETWEEN STRINGER 26LH TO 26 RH AT INTERNAL FUSELAGE. FRAME IN STA. FS=847 +48 BETWEEN STRINGER 26LH TO 26 RH AT INTERNAL FUSELAGE WAS REPAIRED PER E.A 81-2021-010 REV. IR