What was found
FLOOR PANEL 211JF IS CRACKED. REPAIRED THE FLOOR PANEL IAW SRM 51-70-11, REPAIR 1 FIG 201. FABRICATED A REPAIR DOUBLER. APPLIED ALODINE AND PRIMER IAW SRM 51-22-01 PAGES 2 AND 3.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FLOOR PANEL 211JF IS CRACKED. REPAIRED THE FLOOR PANEL IAW SRM 51-70-11, REPAIR 1 FIG 201. FABRICATED A REPAIR DOUBLER. APPLIED ALODINE AND PRIMER IAW SRM 51-22-01 PAGES 2 AND 3.