What was found
CORROSION ON FUSELAGE SKIN 25 PERCENT LOBE OF MATERIAL BETWEEN STR 25R-26R, BS 360. CUT OUT CORROSION, INSTALLED DOUBLER AND FILLER ON OUTSIDE OF SKIN EXTENDING 3 ROWS BELOW SKIN LAP PER EA 7-5330-29666. DATED 9/18/98 AND SRM 53-30-3.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CORROSION ON FUSELAGE SKIN 25 PERCENT LOBE OF MATERIAL BETWEEN STR 25R-26R, BS 360. CUT OUT CORROSION, INSTALLED DOUBLER AND FILLER ON OUTSIDE OF SKIN EXTENDING 3 ROWS BELOW SKIN LAP PER EA 7-5330-29666. DATED 9/18/98 AND SRM 53-30-3.