What was found
C-CHECK - RT I/B FLAP JOINT INNER RIB SHOWS 4 EA CRACKS 1 INCH AT XW 129.000. PERFORMED STOP HOLE, FABRICATED REINFORCING ANGLE, AND INSTALLED REINFORCING ANGLE IAW SRM 57-2-0 FIG 2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
C-CHECK - RT I/B FLAP JOINT INNER RIB SHOWS 4 EA CRACKS 1 INCH AT XW 129.000. PERFORMED STOP HOLE, FABRICATED REINFORCING ANGLE, AND INSTALLED REINFORCING ANGLE IAW SRM 57-2-0 FIG 2.