What was found
UPON REMOVAL OF RT WING L/E UPPER SURFACE FIXED PANEL NR 611CT FOUND D BEAM UPPER CHORD CRACK. REPAIRED PER SRM 57-20-03, FIGURE 7. COMPLIED WITH EN 1100-10.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
UPON REMOVAL OF RT WING L/E UPPER SURFACE FIXED PANEL NR 611CT FOUND D BEAM UPPER CHORD CRACK. REPAIRED PER SRM 57-20-03, FIGURE 7. COMPLIED WITH EN 1100-10.