What was found
DURING HMV, CRACK INTERNAL STRUCTURES SUPPORT WEB LOCATED CENTER WING TO FUSELAGE FAIRING AREA ON LOWER FUSELAGE, REF AEROMAN N/R 2020-393373 WO 2020 368/1. PERFORMED PERMENANT REPAIR TO CENTER FUSELAGE II WF RT REAR WEB CRACK AND CORROSION, PER AEROMAN EA53-0802-20, EDT2020-190-035571-A AND EC NR E20-834-01. THIS IS CLASSIFIED AS A MAJOR REPAIR.