What was found
INSPECTION FOUND A 0.5 INCH CRACK IN FUSELAGE SKIN AT STA 727D +3 BELOW STRINGER 23R. A DOUBLER WAS INSTALLED IAW ECRA 5330-03730 AND SRM 53-00-01, FIGURE 201, REPAIR 31.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 0.5 INCH CRACK IN FUSELAGE SKIN AT STA 727D +3 BELOW STRINGER 23R. A DOUBLER WAS INSTALLED IAW ECRA 5330-03730 AND SRM 53-00-01, FIGURE 201, REPAIR 31.