What was found
ON 2C CHECK, THE FUSELAGE FLOOR SUPPORT STRUCTURE BUTT STRAP WAS FOUND TO BE CORRODED. THE PART WAS REPLACED PER SRM CHAPTER 51, STANDARD PRACTICES AND AERODESIGN REPORT NR 2177-1, REV IR DATED 1-17-97.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
ON 2C CHECK, THE FUSELAGE FLOOR SUPPORT STRUCTURE BUTT STRAP WAS FOUND TO BE CORRODED. THE PART WAS REPLACED PER SRM CHAPTER 51, STANDARD PRACTICES AND AERODESIGN REPORT NR 2177-1, REV IR DATED 1-17-97.