As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
UPON REMOVAL OF R3 DOOR SCUFF PLATE FOUND L-28 WITH 3 EA LOCATIONS CORROSION ON FUSELAGE FROM STA 1260-1302. CORRODED LONGERON 28 RT AT STA 1260 TO STA 1302. R & R IAW SRM 51-33-01 REVISION 42. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 109.