What was found
DURING HEAVY CHECK MAINTENANCE FOUND CORROSION INTERNAL FUSELAGE FRAME 88 ON STRINGER 27R. PERFORMED STRINGER 28R SPLICE REPAIR BETWEEN FRAME 86/87 AND FRAME 90 REF SRM 53-23-03/REPAIR 03. A/C REMAINS IN CHECK.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING HEAVY CHECK MAINTENANCE FOUND CORROSION INTERNAL FUSELAGE FRAME 88 ON STRINGER 27R. PERFORMED STRINGER 28R SPLICE REPAIR BETWEEN FRAME 86/87 AND FRAME 90 REF SRM 53-23-03/REPAIR 03. A/C REMAINS IN CHECK.