What was found
FOUND DURING MV4 VISIT, .75 INCH CRACK AT I/B UPPER CORNER NR 5 L/E FLAP ACT ATTACH ANGLE. REMOVED L/E SUPPORT ROD AND INSTALLED DOUBLER PER MM 57-20-21 FIG 807. INSTALLED L/E SUPPORT ROD.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FOUND DURING MV4 VISIT, .75 INCH CRACK AT I/B UPPER CORNER NR 5 L/E FLAP ACT ATTACH ANGLE. REMOVED L/E SUPPORT ROD AND INSTALLED DOUBLER PER MM 57-20-21 FIG 807. INSTALLED L/E SUPPORT ROD.