What was found
DURING HMV, CORROSION WAS FOUND ON FUSELAGE SKIN UNDER FILLET PANEL FAIRING RUBSTRIPS BETWEEN STA Y=763-826 AND LONGERON 25 RT-30. FUSELAGE SKIN BLENDED OUT. INSTALLED DOUBLER REPAIR IAW SRM 53-04 PARA 57.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING HMV, CORROSION WAS FOUND ON FUSELAGE SKIN UNDER FILLET PANEL FAIRING RUBSTRIPS BETWEEN STA Y=763-826 AND LONGERON 25 RT-30. FUSELAGE SKIN BLENDED OUT. INSTALLED DOUBLER REPAIR IAW SRM 53-04 PARA 57.