What was found
INTERNAL FUSELAGE SKIN HAS LIGHT CORROSION PITTING THAT WAS HIDDEN BY FAILSAFE STRAP, ADJACENT TO PICKLE FORK FITTING. REMOVED CORROSION IAW B767 SRM 51-10-02. REPAIRED AREA IAW REA B653-60345-MR, ACFT WAS GROUNDED.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INTERNAL FUSELAGE SKIN HAS LIGHT CORROSION PITTING THAT WAS HIDDEN BY FAILSAFE STRAP, ADJACENT TO PICKLE FORK FITTING. REMOVED CORROSION IAW B767 SRM 51-10-02. REPAIRED AREA IAW REA B653-60345-MR, ACFT WAS GROUNDED.