What was found
PIT - DURING Q-1/C-6 INSPECTION, FOUND .5 INCH CRACK AT CANTED FRAME 1485 AT LONGERON 7L. STOPPED DRILLED CRACK AND INSTALLED DOUBLER REPAIR PER SRM 53-14-4 FIG 3. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
PIT - DURING Q-1/C-6 INSPECTION, FOUND .5 INCH CRACK AT CANTED FRAME 1485 AT LONGERON 7L. STOPPED DRILLED CRACK AND INSTALLED DOUBLER REPAIR PER SRM 53-14-4 FIG 3. (M)