What was found
DURING SCHEDULED C-1 CHECK, FOUND RT FUSELAGE EXTERIOR CHINE ANGLE WITH STRESS CORROSION CRACKING AT BS 287E TO 297E. REPAIRED IAW SMP 583, SRM 51-60 & 51-70.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING SCHEDULED C-1 CHECK, FOUND RT FUSELAGE EXTERIOR CHINE ANGLE WITH STRESS CORROSION CRACKING AT BS 287E TO 297E. REPAIRED IAW SMP 583, SRM 51-60 & 51-70.