What was found
DURING SHOP INSPECTION, FOUND CRACK IN L/E SKIN AT 153 IN FROM O/B END. RIGHT WING FLAP PANEL. REPAIRED PER SRM 57-50-4 FIG 1.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING SHOP INSPECTION, FOUND CRACK IN L/E SKIN AT 153 IN FROM O/B END. RIGHT WING FLAP PANEL. REPAIRED PER SRM 57-50-4 FIG 1.