What was found
CORROSION ON FLOOR PANEL INTERNAL SKIN FRAME 30+18 BETWEEN STRINGERS 43-44L, FOUND WITHIN LIMITS IAW SRM 53-21-11, TABLE 101, PARA 4E DIAGRAM 105.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CORROSION ON FLOOR PANEL INTERNAL SKIN FRAME 30+18 BETWEEN STRINGERS 43-44L, FOUND WITHIN LIMITS IAW SRM 53-21-11, TABLE 101, PARA 4E DIAGRAM 105.