What was found
(CAN) ON 100 HOUR INSPECTION, TAILBOOM ATTACHMENT BOLT AT 12 O'CLOCK POSITION WAS UNDERTORQUE. FUSELAGE REAR FRAME SUPPORT WAS CRACKED APPROXIMATELY 1 INCH AT EACH OF 3 LOCATIONS. 12, 2, AND 3 O'CLOCK POSITIONS.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
(CAN) ON 100 HOUR INSPECTION, TAILBOOM ATTACHMENT BOLT AT 12 O'CLOCK POSITION WAS UNDERTORQUE. FUSELAGE REAR FRAME SUPPORT WAS CRACKED APPROXIMATELY 1 INCH AT EACH OF 3 LOCATIONS. 12, 2, AND 3 O'CLOCK POSITIONS.