As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
SAL - Q2 - MAJOR REPAIR - CRACK IN FUSELAGE SKIN AT FORWARD ENTRY DOOR LOWER HINGE CUTOUT BETWEEN BS 294.5 TO BS 312 & BETWEEN S12L TO S14L. REPAIRED FUSELAGE SKIN AT FORWARD ENTRY DOOR LOWER HINGE CUTOUT BETWEEN BS 294.5 TO BS 312 & BETWEEN S12L TO S14L IAW EA 3132666A.