What was found
A .25 INCH CRACK AT NS 222 AND .5 INCH CRACK AT NS 236. DISCOVERED AFTER REMOVAL OF DOUBLER NR 1 PYLON. REPAIRED PER BOEING SRM 54-30-03 PAGE 113.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
A .25 INCH CRACK AT NS 222 AND .5 INCH CRACK AT NS 236. DISCOVERED AFTER REMOVAL OF DOUBLER NR 1 PYLON. REPAIRED PER BOEING SRM 54-30-03 PAGE 113.