What was found
DURING INSPECTION, FOUND CRACK IN RUDDER SKIN .5 INCH LENGTH ON LT SIDE 4 AFT OF CENTERLINE STA ZR 26.043. MAINTENANCE INSTALLED DOUBLER REPAIR IAW SRM 55-01 FIG 2. RECALCULATED BALANCE AND RETURNED A/C TO SERVICE.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING INSPECTION, FOUND CRACK IN RUDDER SKIN .5 INCH LENGTH ON LT SIDE 4 AFT OF CENTERLINE STA ZR 26.043. MAINTENANCE INSTALLED DOUBLER REPAIR IAW SRM 55-01 FIG 2. RECALCULATED BALANCE AND RETURNED A/C TO SERVICE.