What was found
DURING M-CHECK, FOUND FLOOR PANEL 26, CORROSION AT CORNER BOTTOM SECTION. CORRODED OUT OF LIMITS IAW SRM 53-01, FIG 1. REPAIRED IAW 51-70-4, FIG 1. R & R DOUBLER IAW SRM 51-30-2 AND 51-70-4.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING M-CHECK, FOUND FLOOR PANEL 26, CORROSION AT CORNER BOTTOM SECTION. CORRODED OUT OF LIMITS IAW SRM 53-01, FIG 1. REPAIRED IAW 51-70-4, FIG 1. R & R DOUBLER IAW SRM 51-30-2 AND 51-70-4.