As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(CAN) DURING THE ACCOMPLISHMENT OF C-CHECK, THE NOSE ACTUATOR FUSELAGE FITTING WAS FOUND WITH (2) BOLTS SHEARED. SB 8-53-50 FOR THIS FAILURE. THE CUT IN S/N WAS 403 AND OUR A/C WAS S/N:410. THE MODIFICATION 8/2140 WAS TRULY ACCOMPLISHED. THE FITTING WAS INSTALLED WITH BIGGER BOLTS BUT (2) OF THOSE BOLTS WERE SHEARED. (TC NR 20070305002)