What was found
C3 CHECK - CRACK ON FLOOR PANEL ATTACH ANGLE BETWEEN BS 1620 TO BS 1640, BL 0. REPLACED FLOOR PANEL ATTACH ANGLE BETWEEN BS 1620 TO BS 1640, BL 0 IAW B757 SRM 51-40-02 FIG 5.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
C3 CHECK - CRACK ON FLOOR PANEL ATTACH ANGLE BETWEEN BS 1620 TO BS 1640, BL 0. REPLACED FLOOR PANEL ATTACH ANGLE BETWEEN BS 1620 TO BS 1640, BL 0 IAW B757 SRM 51-40-02 FIG 5.