What was found
RH WING INBOARD MAIN FLAP L/E HOLE (FROM 26 IN RH EDGE)(<P>RH WING INBOARD MAIN FLAP, AFT FLAP WAS REPAIRED IAW SRM 57-53-01-2R-1 FIG 201 SHEET 5 PAGE 2-3, 6 AND SRM 51-70-17-0G-0 PAR 4 B FIG 24 PAGE 14, 55 REV.124 DEC 15/2023</P>)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
RH WING INBOARD MAIN FLAP L/E HOLE (FROM 26 IN RH EDGE)(<P>RH WING INBOARD MAIN FLAP, AFT FLAP WAS REPAIRED IAW SRM 57-53-01-2R-1 FIG 201 SHEET 5 PAGE 2-3, 6 AND SRM 51-70-17-0G-0 PAR 4 B FIG 24 PAGE 14, 55 REV.124 DEC 15/2023</P>)