What was found
DURING ANNUAL INSPECTION, A CRACK WAS FOUND IN THE RUDDER PEDAL ASSEMBLY CONNECTING TUBE. THE CRACK WAS APPROXIMATELY .25 INCH LONG AND LOCATED ON THE AFT SIDE OF A TUBE WELD. (REF: AC 43-16-, ALERT NR 198, JANUARY, 1995, PAGE 11.)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING ANNUAL INSPECTION, A CRACK WAS FOUND IN THE RUDDER PEDAL ASSEMBLY CONNECTING TUBE. THE CRACK WAS APPROXIMATELY .25 INCH LONG AND LOCATED ON THE AFT SIDE OF A TUBE WELD. (REF: AC 43-16-, ALERT NR 198, JANUARY, 1995, PAGE 11.)