What was found
INSPECTION FOUND A 1.25 INCH CRACK IN FUSELAGE SKIN JUST FORWARD OF LOWER HINGE OF L-1 DOOR. THE CRACKED AREA OF SKIN WAS CUT OUT, FILLER AND DOUBLER WERE FABRICATED AND INSTALLED IAW WORK CONTROL CARD M AND E NR 07-5310-1-0100.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 1.25 INCH CRACK IN FUSELAGE SKIN JUST FORWARD OF LOWER HINGE OF L-1 DOOR. THE CRACKED AREA OF SKIN WAS CUT OUT, FILLER AND DOUBLER WERE FABRICATED AND INSTALLED IAW WORK CONTROL CARD M AND E NR 07-5310-1-0100.