What was found
DURING OP 16 MAINT CHECK, NR 2 PYLON HAD A CRACK IN THE WEB 9.5 INCHES OTBD OF THE FUSELAGE SKIN, TOP OF PYLON AT STA 1038. REPLACED PART PER DAC PRINT INSTALLATION 9915501, INSTALLED RIB 9915501-2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING OP 16 MAINT CHECK, NR 2 PYLON HAD A CRACK IN THE WEB 9.5 INCHES OTBD OF THE FUSELAGE SKIN, TOP OF PYLON AT STA 1038. REPLACED PART PER DAC PRINT INSTALLATION 9915501, INSTALLED RIB 9915501-2.