What was found
INSPECTION FOUND A 4 INCH CRACK IN FUSELAGE SKIN AT STA 837-867, STRINGER 1. A REPAIR WAS INSTALLED IAW SRM 53-00-01, FIGURE 201.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 4 INCH CRACK IN FUSELAGE SKIN AT STA 837-867, STRINGER 1. A REPAIR WAS INSTALLED IAW SRM 53-00-01, FIGURE 201.