What was found
SUPPLEMENTAL INFORMATION: 7.(C) CRACK LENGTH SHOULD BE .375 AND 7.(D) NUMBER OF CRACKS SHOULD BE 1
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
SUPPLEMENTAL INFORMATION: 7.(C) CRACK LENGTH SHOULD BE .375 AND 7.(D) NUMBER OF CRACKS SHOULD BE 1