What was found
FR 38 BETWEEN STR 20-21L CORRODED. REMOVED CORROSION ON FR38 BTW STR 20-21L AS PER SRM 51-21-42 AND WITHIN LIMITS AS PER SRM 53-61-00 MATERIAL THICKNESS: 0.063 MATERIAL REMOVED: 0.003 WITHIN LIMITS AS PER SRM: 53-61-00 FIG 301.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FR 38 BETWEEN STR 20-21L CORRODED. REMOVED CORROSION ON FR38 BTW STR 20-21L AS PER SRM 51-21-42 AND WITHIN LIMITS AS PER SRM 53-61-00 MATERIAL THICKNESS: 0.063 MATERIAL REMOVED: 0.003 WITHIN LIMITS AS PER SRM: 53-61-00 FIG 301.