What was found
CRACK ON SKIN NEXT TO HOLD AT LT FLOOR PANEL NR 389A. FLOOR PANEL WAS REPAIRED IAW SRM 53-01, FIG 4 AND 51-10-3 PAR 14 AND 21.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK ON SKIN NEXT TO HOLD AT LT FLOOR PANEL NR 389A. FLOOR PANEL WAS REPAIRED IAW SRM 53-01, FIG 4 AND 51-10-3 PAR 14 AND 21.