What was found
PIT - DURING Q-4/CX-6 CHECK INSPECTION, FOUND A .25 INCH CRACK RIGHT INBOARD WEB LEADING EDGE TO HORIZONTAL STABILIZER FROM SPAR. INSTALLED DOUBLER REPAIR IAW SRM 55-01 FIG 5. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
PIT - DURING Q-4/CX-6 CHECK INSPECTION, FOUND A .25 INCH CRACK RIGHT INBOARD WEB LEADING EDGE TO HORIZONTAL STABILIZER FROM SPAR. INSTALLED DOUBLER REPAIR IAW SRM 55-01 FIG 5. (M)