What was found
AT C-CHECK, COCKPIT HAD HEAVY CORROSION BETWEEN FINGER DOUBLER AND PRESSURE PANEL BELOW COCKPIT FLOOR LEFT SIDE OF LBL 60, FS 8-12. INSTALLED FRAME REPAIR PER ROD SKETCH 96-05-16-00.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AT C-CHECK, COCKPIT HAD HEAVY CORROSION BETWEEN FINGER DOUBLER AND PRESSURE PANEL BELOW COCKPIT FLOOR LEFT SIDE OF LBL 60, FS 8-12. INSTALLED FRAME REPAIR PER ROD SKETCH 96-05-16-00.