What was found
RIGHT UPPER AFT HORIZONTAL STABILIZER SKIN PANEL INBD AFT CORNER HAS A .400 INCH CRACK. CRACK STOP DRILLED IAW WC 55X1203ALI-P4 FIGURE 2 TABLE 1. CRACK FOUND TO BE LIMITS. TRACKING TO BE ACCOMPLISHED ON WC AT 80 FLIGHT HOUR INTERVALS.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
RIGHT UPPER AFT HORIZONTAL STABILIZER SKIN PANEL INBD AFT CORNER HAS A .400 INCH CRACK. CRACK STOP DRILLED IAW WC 55X1203ALI-P4 FIGURE 2 TABLE 1. CRACK FOUND TO BE LIMITS. TRACKING TO BE ACCOMPLISHED ON WC AT 80 FLIGHT HOUR INTERVALS.