What was found
(CAN) CRACK WAS DETECTED ABOVE THE RT TOP FWD ATTACH POINT, BETWEEN THE TOP ATTACH BOLT AND THE RADIUS OF THE SPAR FLANGE. THIS UNIT HAD A TOTAL OF 963.4 HRS SINCE INSTALLATION. (TC 20100204004)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
(CAN) CRACK WAS DETECTED ABOVE THE RT TOP FWD ATTACH POINT, BETWEEN THE TOP ATTACH BOLT AND THE RADIUS OF THE SPAR FLANGE. THIS UNIT HAD A TOTAL OF 963.4 HRS SINCE INSTALLATION. (TC 20100204004)