What was found
DELAMINATED COMPOSITE MATERIAL, PUNCTURES ON CHANNELS AND CORROSION ON STRAP AT FLOOR PANEL 200A. THE FLOOR PANEL AND CHANNELS WERE REPAIRED IAW SRM 51-70-1D, PAR. 10. AND DWG 9952523, REV Y.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DELAMINATED COMPOSITE MATERIAL, PUNCTURES ON CHANNELS AND CORROSION ON STRAP AT FLOOR PANEL 200A. THE FLOOR PANEL AND CHANNELS WERE REPAIRED IAW SRM 51-70-1D, PAR. 10. AND DWG 9952523, REV Y.