As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
SURFACE HFEC INSPECTION FOUND 01EA CRACK APPROX.0.650 INCH IN LENGTH ON THE EXTERNAL SURFACE OF THE FUSELAGE SKIN AROUND THE 01EA HOLE COMMON TO THE RIGHT SIDE UNDERWING LONGERON AND FUSELAGE SKIN AS MARK AS PER W/C EO G-5310- E0332629 K P6 STEP 9. C. COMPLIED WITH EO: G-5310-E0332629K P6 , STEP 11. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. (THE CORRECT NON ROUTINE # IS N00064)