What was found
DURING HEAVY CHECK MAINTENANCE FOUND CRACK FOUND ON FWD FUSELAGE COCKPIT UNDER FLOOR CONSOLE ANGLE AT FR 12 AND BL 0. FWD FUSELAGE COCKPIT UNDER FLOOR CONSOLE ANGLE AT FR 12 AND BL 0 REPLACED, IAW SRM 51-41-01. 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 CRACK FOUND ON FWD FUSELAGE COCKPIT UNDER FLOOR CONSOLE ANGLE AT FR 12 AND BL 0. FWD FUSELAGE COCKPIT UNDER FLOOR CONSOLE ANGLE AT FR 12 AND BL 0 REPLACED, IAW SRM 51-41-01. A/C REMAINS IN CHECK.