What was found
DURING SHOP INSPECTION, THE AFT LOWER CHORD ANGLE WAS FOUND CRACKED 36 INCHES FROM I/B END OF FLAP. THE ANGLE WAS REPAIRED BY STOP DRILLING THE CRACK AND INSTALLING A DOUBLER PER MM 57-52-0 FIG 802.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING SHOP INSPECTION, THE AFT LOWER CHORD ANGLE WAS FOUND CRACKED 36 INCHES FROM I/B END OF FLAP. THE ANGLE WAS REPAIRED BY STOP DRILLING THE CRACK AND INSTALLING A DOUBLER PER MM 57-52-0 FIG 802.