What was found
DURING C-CHECK AND COMPLIANCE WITH AD 92-22-08, FOUND VERTICAL STABILIZER LEADING EDGE RIB CRACKED, FOURTH FROM BOTTOM LEFT. REPAIRED IAW SUPPLEMENTAL SRM DWG K05159.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING C-CHECK AND COMPLIANCE WITH AD 92-22-08, FOUND VERTICAL STABILIZER LEADING EDGE RIB CRACKED, FOURTH FROM BOTTOM LEFT. REPAIRED IAW SUPPLEMENTAL SRM DWG K05159.