What was found
RH RIB HAS A CRACK AT BODY STA X = 15315.0 PANELS FWD OF VENTRICLE TANK, AFT WHEEL CELL. CRACK IS AT LWR CENTER. REMOVED AND REPLACED NEW RIB.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
RH RIB HAS A CRACK AT BODY STA X = 15315.0 PANELS FWD OF VENTRICLE TANK, AFT WHEEL CELL. CRACK IS AT LWR CENTER. REMOVED AND REPLACED NEW RIB.