What was found
WHILE PERFORMING AN INSPECTION IN THE VERT STAB, THE RIB FLANGES AT CANTED STAB STA 39.289 AND STA 54.026 WERE FOUND CRACKED. REPAIRED FLANGE IN ACCORDANCE WITH BEECH STRUCTURAL MANUAL P/N 114-590021-9, 51-70-03.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
WHILE PERFORMING AN INSPECTION IN THE VERT STAB, THE RIB FLANGES AT CANTED STAB STA 39.289 AND STA 54.026 WERE FOUND CRACKED. REPAIRED FLANGE IN ACCORDANCE WITH BEECH STRUCTURAL MANUAL P/N 114-590021-9, 51-70-03.