As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LH HORIZONTAL STABILIZER LEADING EDGE PANEL; LE STA 86.66 (2ND RIB FROM INBOARD EDGE) RIB INNER CHORD ANGLE CRACKED AT UPPER AFT FASTENER HOLE; MARKED. / REPLACED NEW RIB ON L/H HORIZONTAL STAB LE ACCESS PANEL ( #2 FROM INBD SIDE ) I.A.W B737-700 SRM 51-40-02-0G.