What was found
DURING SHOP INSPECTION, THE AFT CHORD ANGLE WAS FOUND CRACKED AT 2 PLACES APPROX 34 INCHES FROM I/B END OF FLAP. THE ANGLE WAS REPAIRED PER MM 57-52-00, FIG 802 BY REPLACING A SECTION OF THE ANGLE AND INSTALLING A SPLICE DOUBLER.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING SHOP INSPECTION, THE AFT CHORD ANGLE WAS FOUND CRACKED AT 2 PLACES APPROX 34 INCHES FROM I/B END OF FLAP. THE ANGLE WAS REPAIRED PER MM 57-52-00, FIG 802 BY REPLACING A SECTION OF THE ANGLE AND INSTALLING A SPLICE DOUBLER.