What was found
PIT - DURING Q-1 INSPECTION, FOUND .5 INCH CRACK IN STRINGER NR 68 RIGHT SIDE 4 INCHES AFT OF FRAME 3870. INSTALLED DOUBLER REPAIR PER SRM 51-70-06 FIG 202. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
PIT - DURING Q-1 INSPECTION, FOUND .5 INCH CRACK IN STRINGER NR 68 RIGHT SIDE 4 INCHES AFT OF FRAME 3870. INSTALLED DOUBLER REPAIR PER SRM 51-70-06 FIG 202. (M)