What was found
DURING EXIT CHECK, INSPECTION REPORTED FLOOR SUPPORT ANGLE CRACKED FROM STA. 380 TO STA. 400, BL O, WL 208. FABRICATED AND REPLACED ANGLE PER SRM 51-10-02, 53-30-01, 53-30-51, FIG. 1, AND 51-20-01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING EXIT CHECK, INSPECTION REPORTED FLOOR SUPPORT ANGLE CRACKED FROM STA. 380 TO STA. 400, BL O, WL 208. FABRICATED AND REPLACED ANGLE PER SRM 51-10-02, 53-30-01, 53-30-51, FIG. 1, AND 51-20-01.