What was found
LEFT HORIZONTAL STAB SKIN PANEL AFT SECTION (UPPER) SHOWS A CRACK INDICATION BETWEEN THE 2 BLACK DOTS APPROX 0.430 LONG AND 0.875 OFF THE AFT EDGE OF THE SKIN PANEL. REPAIRED SKIN PANEL PER EA 8-5510-123505.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LEFT HORIZONTAL STAB SKIN PANEL AFT SECTION (UPPER) SHOWS A CRACK INDICATION BETWEEN THE 2 BLACK DOTS APPROX 0.430 LONG AND 0.875 OFF THE AFT EDGE OF THE SKIN PANEL. REPAIRED SKIN PANEL PER EA 8-5510-123505.