What was found
THE FUSELAGE SKIN HAD A 2 IN CRACK AT THE UPPER FORWARD CORNER OF THE L1 DOOR OPENING. THE CRACKED SKIN WAS CUT OUT AND A REPAIR DOUBLER WAS INSTALLED. REF. 6-089732-12AD
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
THE FUSELAGE SKIN HAD A 2 IN CRACK AT THE UPPER FORWARD CORNER OF THE L1 DOOR OPENING. THE CRACKED SKIN WAS CUT OUT AND A REPAIR DOUBLER WAS INSTALLED. REF. 6-089732-12AD