What was found
INSPECTION FOUND FUSELAGE SKIN CORRODED UNDER KEEL BEAM AREA AT BS 676, LONGERON 30. A PERMANENT REPAIR DOUBLER AND FILLER WERE INSTALLED IAW ENGINEERING ORDER 07512 AND SRM 53-04, FIGURE 38, SHEET 3.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND FUSELAGE SKIN CORRODED UNDER KEEL BEAM AREA AT BS 676, LONGERON 30. A PERMANENT REPAIR DOUBLER AND FILLER WERE INSTALLED IAW ENGINEERING ORDER 07512 AND SRM 53-04, FIGURE 38, SHEET 3.