What was found
PIT - DURING Q-1/C-3 CHECK INSPECTION, FOUND .75 INCH VERTICAL CRACK AFT SIDE OF STA 1388, CANTED FRAME, IN ANGLE ON LEFT FRONT SPAR OF VERTICAL STABILIZER. INSTALLED ANGLE REPAIR PER SRM 55-02, FIGURE 26. (X)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
PIT - DURING Q-1/C-3 CHECK INSPECTION, FOUND .75 INCH VERTICAL CRACK AFT SIDE OF STA 1388, CANTED FRAME, IN ANGLE ON LEFT FRONT SPAR OF VERTICAL STABILIZER. INSTALLED ANGLE REPAIR PER SRM 55-02, FIGURE 26. (X)