As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
UPON COMPLIANCE WITH AD, DETECTED A CRACK COMPLETELY THROUGH CAST WEB. INSTALLED NEW CARRIAGE ASSEMBLY PN T700A5755098001. NEW PART WEB THICKNESS IS 3X THICKER. POSSIBLE CAUSE; HIGH KIT FLAP OPERATING SPEED. REPLACEMENT PART APPEARS TO BE REINFORCED IN AFFECTED AREA.