As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING ACCOMPLISHING OF EO F-5330-7-5004 PT1 STEP 4.B OPEN HOLE HFEC INSPECTION QTY 02 HOLES FOUND CRACK APPROX MORE THAN 0.020" DEPTH ON FUSELAGE SKIN AT L1 DOOR CUTOUT UPPER FWD AREA. CRACKED SKIN ON L1 DOOR CUTOUT REPAIRED AS PER EA F-5330-137686 (EXISTING REPAIR - L1 DOOR UPPER FWD CORNER CRACK REPAIR - DEVIATION TO EO F-5330-7-5004). REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100.