As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION TYPE:C2, RT FUSELAGE EXTERNAL SKIN AT STA 902 HAS INTERGRANULAR CORROSION BELOW CUSP LINE ADJACENT TO SKIN SPLICE. BLENDED OUT AREA IAW REO-G07351. ALODINED AND PRIMED IAW DC8 SRM 51-1 -8. INSTALLED FAST IAW DAC DWG 5750554 & DC8 SRM 51-1-20D & 51-9-0.