What was found
DURING C/W SB 198A, PART I, CRACKS WERE FOUND RT FWD SCREW HOLE IN LEFT AND RIGHT RIBS ON BOTH TRIM TABS. FOUND NO OTHER DAMAGE AND RIBS WERE REPAIRED/MODIFIED PER SB 198A, PART II.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING C/W SB 198A, PART I, CRACKS WERE FOUND RT FWD SCREW HOLE IN LEFT AND RIGHT RIBS ON BOTH TRIM TABS. FOUND NO OTHER DAMAGE AND RIBS WERE REPAIRED/MODIFIED PER SB 198A, PART II.