What was found
DURING SHOP INSPECTION, THE FLAP REAR CHORD ANGLE WAS FOUND CRACKED 32 AND 37 FROM THE IB END. THE ANGLE WAS REPAIRED BY INSTALLING A DOUBLER PER 727 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 FLAP REAR CHORD ANGLE WAS FOUND CRACKED 32 AND 37 FROM THE IB END. THE ANGLE WAS REPAIRED BY INSTALLING A DOUBLER PER 727 MM 57-52-0, FIG 802.