What was found
AT C-CHECK, AFT FUSELAGE SECTION 36 LONGERON SPLICE AFT FITTING CRACKED 2 INCHES BETWEEN STA 1690 AND STA 1702. REMOVED AND REPLACED FITTING IAW SRM 51-1-8 PG 12B. REF: N/R 5483.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AT C-CHECK, AFT FUSELAGE SECTION 36 LONGERON SPLICE AFT FITTING CRACKED 2 INCHES BETWEEN STA 1690 AND STA 1702. REMOVED AND REPLACED FITTING IAW SRM 51-1-8 PG 12B. REF: N/R 5483.