What was found
MAIN CABIN FLOOR SUPPORT ANGLE HAS CORROSION FROM STA 180 TO 200 AT RBL 53. REMOVED CORROSION AND FOUND OUT LIMITS IAW SRM 51-10-03 AND 53-01, FIG 1. REPLACED FLOOR SUPPORT IAW SRM 51-30-2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
MAIN CABIN FLOOR SUPPORT ANGLE HAS CORROSION FROM STA 180 TO 200 AT RBL 53. REMOVED CORROSION AND FOUND OUT LIMITS IAW SRM 51-10-03 AND 53-01, FIG 1. REPLACED FLOOR SUPPORT IAW SRM 51-30-2.