What was found
FRAME 39 CORRODED BETWEEN STR 21 RT TO 21 LT. REPAIRED AS PER SRM 53-61-40 FIG 415 MATERIAL THICKNESS 0.080 MATERIAL REMOVED 0.075 OUT OF LIMITS AS PER SRM 53-61-00 FIG 307
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FRAME 39 CORRODED BETWEEN STR 21 RT TO 21 LT. REPAIRED AS PER SRM 53-61-40 FIG 415 MATERIAL THICKNESS 0.080 MATERIAL REMOVED 0.075 OUT OF LIMITS AS PER SRM 53-61-00 FIG 307