What was found
FUSELAGE FRAME B STA 880 RT FOUND CRACKED AT CUTOUT FOR STR 33 (TOP CORNER). REPAIRED IAW B747 SRM 53-10-04. REPAIR ANGLE USED 7075-T6 0.063.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE FRAME B STA 880 RT FOUND CRACKED AT CUTOUT FOR STR 33 (TOP CORNER). REPAIRED IAW B747 SRM 53-10-04. REPAIR ANGLE USED 7075-T6 0.063.