What was found
DURING INSPECTION PER PIPER SB 998A, FOUND CRACKS IN BOTH UPPER AND LOWER FLANGE RADIUS AS DESCRIBED. NO CRACKS IN AREA OF OUTBOARD HINGE ATTACH REINFORCEMENT.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING INSPECTION PER PIPER SB 998A, FOUND CRACKS IN BOTH UPPER AND LOWER FLANGE RADIUS AS DESCRIBED. NO CRACKS IN AREA OF OUTBOARD HINGE ATTACH REINFORCEMENT.