As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
UPON REMOVAL OF COUNTER BALANCE WEIGHT CORROSION WAS FOUND ON THE UPPER EDGE OF BALANCE ARM. CORROSION SPOT 1 IS 2.5' FROM R/H END AND .200' OF EDGE CORNER REMOVED. CORROSION SPOT 2 ID 4' FROM R/H END AND 300' OF EDGE OF CORNER REMOVED (TRANSFERRED FROM NRC #G483103 / BLENDED AREA IAW SRM 51-41-02 & ACCOMPLISHED EA 1-755-3798 SEE ATTACHED SAM 326 FOR INDIVIDUAL SIGN OFFS