What was found
MAIN CABIN INNER ANGLE HAS CORROSION AT BS 758, RBL 65. REMOVED CORROSION IAW SRM 53-30-13, ALLOWABLE DAMAGE 1 PG 105, DETAIL VIII. R & R INNER ANGLE FROM BS 740 TO 900 IAW SRM 51-40-02, PAGE 7. C
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
MAIN CABIN INNER ANGLE HAS CORROSION AT BS 758, RBL 65. REMOVED CORROSION IAW SRM 53-30-13, ALLOWABLE DAMAGE 1 PG 105, DETAIL VIII. R & R INNER ANGLE FROM BS 740 TO 900 IAW SRM 51-40-02, PAGE 7. C