What was found
CRACKS IN STABILATOR MAIN SPAR ADJACENT TO FUSELAGE HINGE ATTACHMENT FITTING. THIS AIRCRAFT IS USED FOR FLIGHT TRAINING. CRACKS POSSIBLY DUE TO FATIGUE. RECOMMEND DETAILED INSPECTION OF THIS AREA AT EACH INSPECTION INTERVAL.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACKS IN STABILATOR MAIN SPAR ADJACENT TO FUSELAGE HINGE ATTACHMENT FITTING. THIS AIRCRAFT IS USED FOR FLIGHT TRAINING. CRACKS POSSIBLY DUE TO FATIGUE. RECOMMEND DETAILED INSPECTION OF THIS AREA AT EACH INSPECTION INTERVAL.