What was found
MAIN CABIN FLOOR PANEL CF AT FRAME C 11 A, LOWER SURFACE IS CRACKED. REPAIRED AS REQUIRED IAW ARM 53-10-20; FIG 202.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
MAIN CABIN FLOOR PANEL CF AT FRAME C 11 A, LOWER SURFACE IS CRACKED. REPAIRED AS REQUIRED IAW ARM 53-10-20; FIG 202.