What was found
DURING C-CHECK AFT FUSELAGE INSIDE ACCESS 312AR AT FRAME 81, STRINGER 10, RT END CLIP IS CRACKED AT APU FIREWALL. MAINTENANCE R & R FRAME 81, STRINGER 10, RT END CLIP IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING C-CHECK AFT FUSELAGE INSIDE ACCESS 312AR AT FRAME 81, STRINGER 10, RT END CLIP IS CRACKED AT APU FIREWALL. MAINTENANCE R & R FRAME 81, STRINGER 10, RT END CLIP IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.