What was found
(CAN) A 1.5 INCH CRACK WAS FOUND AT THE BOTTOM OF THE STALL STRIP WHICH IS RIVETED TO THE AFT EDGE OF THE RUDDER TRIM TAB. RUDDER ASSEMBLY REPLACED WITH SPARE. (TC NR 20091216007)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
(CAN) A 1.5 INCH CRACK WAS FOUND AT THE BOTTOM OF THE STALL STRIP WHICH IS RIVETED TO THE AFT EDGE OF THE RUDDER TRIM TAB. RUDDER ASSEMBLY REPLACED WITH SPARE. (TC NR 20091216007)