What was found
FUSELAGE SKIN AT L1 DOOR CUTOUT HAS CRACK EMANATING FROM FASTENER HOLE INTO RADIUS OF JAMB. REPAIRED CRACK IAW AWA ER 03-5310-01059-JS1 AND DWG 65C27257-5.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE SKIN AT L1 DOOR CUTOUT HAS CRACK EMANATING FROM FASTENER HOLE INTO RADIUS OF JAMB. REPAIRED CRACK IAW AWA ER 03-5310-01059-JS1 AND DWG 65C27257-5.