What was found
DURING C-CHECK AND COMPLIANCE WITH AD 92-22-08, FOUND VERTICAL STABILIZER REMOVABLE LEADING EDGE RIB CRACKED, SECOND 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 REMOVABLE LEADING EDGE RIB CRACKED, SECOND FROM BOTTOM LEFT. REPAIRED IAW SUPPLEMENTAL SRM DWG K05159.