As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
WHILE PERFORMING HFEC OF DENTED AREA ON LEFT HORIZONTAL LEADING EDGE SKIN SURFACE;NOTE CRACK INDICATION BETWEEN FASTENERS AT DENT EDGE AT RIB AREA AND SKIN PULLED FROM ONE FASTENER. REF EA 1-755-3835 AND / REMOVED AND REPLACED L/H HORIZONTAL STAB LEADING EDGE REF AMM 27-41-21 AND EA 1-A51-0259 P/N OFF/ON:186A1001-15 S/N OFF:230#1 S/N ON:427#1