What was found
INSPECTION TYPE-C, AFT FUSELAGE TAIL SKID FITTING IS CRACKED AT BOTH END BOLT HOLES AT STA 1750 BL 0. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION TYPE-C, AFT FUSELAGE TAIL SKID FITTING IS CRACKED AT BOTH END BOLT HOLES AT STA 1750 BL 0. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.