What was found
FOUND ON CV2 CHECK, (1) .25 INCH VISIBLE CRACK ON NR 5 SLAT L/E RIB O/B OF ACTUATOR ROD. (2) 2.0625 INCH CRACKS ON NR 5 SLAT L/E RIB I/B OF ACTUATOR ROD. REPAIRED PER M/M 57-54-0 PAR 3.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FOUND ON CV2 CHECK, (1) .25 INCH VISIBLE CRACK ON NR 5 SLAT L/E RIB O/B OF ACTUATOR ROD. (2) 2.0625 INCH CRACKS ON NR 5 SLAT L/E RIB I/B OF ACTUATOR ROD. REPAIRED PER M/M 57-54-0 PAR 3.