What was found
FITTING CRACKED MORE THAN 90 PERCENT OF FITTING AT FLAP ATTACH POINT, DEFECT NOTED DURING FLAP OVERHAUL. FLAP RECEIVED FOR OVERHAUL DUE TO AIRCRAFT IN D-CHECK.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FITTING CRACKED MORE THAN 90 PERCENT OF FITTING AT FLAP ATTACH POINT, DEFECT NOTED DURING FLAP OVERHAUL. FLAP RECEIVED FOR OVERHAUL DUE TO AIRCRAFT IN D-CHECK.