What was found
INSPECTION FOUND A .875 INCH CRACK WITH CORROSION IN FUSELAGE SKIN AT BS 2220 BETWEEN STRINGERS 50R AND 51R. A SKIN REPAIR WAS INSTALLED IAW SRM 53-30-03, FIGURE 1 AND THE STRINGERS WERE REPAIRED IAW SRM 53-10-03, FIGURE 1.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A .875 INCH CRACK WITH CORROSION IN FUSELAGE SKIN AT BS 2220 BETWEEN STRINGERS 50R AND 51R. A SKIN REPAIR WAS INSTALLED IAW SRM 53-30-03, FIGURE 1 AND THE STRINGERS WERE REPAIRED IAW SRM 53-10-03, FIGURE 1.