What was found
LEFT HORIZONTAL STAB AFT UPPER SKIN PANEL HAS A SURFACE CRACK .25 LONG FROM AFT EDGE. VERIFIED WITH HFEC. REPAIRED IAW ERA 522297-14, REV O.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LEFT HORIZONTAL STAB AFT UPPER SKIN PANEL HAS A SURFACE CRACK .25 LONG FROM AFT EDGE. VERIFIED WITH HFEC. REPAIRED IAW ERA 522297-14, REV O.