What was found
RT HORIZ STABILIZER L/E INNER RIB CRACKED .5 INCH AT XFS 47.5. STOP DRILLED CRACK, FABRICATED REINFORCING ANGLE, AND INSTALLED ANGLE PER SRM 55-2-0 FIG 2 &51-1-21 PG 1.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
RT HORIZ STABILIZER L/E INNER RIB CRACKED .5 INCH AT XFS 47.5. STOP DRILLED CRACK, FABRICATED REINFORCING ANGLE, AND INSTALLED ANGLE PER SRM 55-2-0 FIG 2 &51-1-21 PG 1.