What was found
INSPECTION FOUND A 2.75 INCH CRACK IN FUSELAGE SKIN AT L-1 DOOR LOWER HINGE CUTOUT. THE CRACKED AREA WAS CUT OUT, A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-2 AND 51-20-4.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 2.75 INCH CRACK IN FUSELAGE SKIN AT L-1 DOOR LOWER HINGE CUTOUT. THE CRACKED AREA WAS CUT OUT, A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-2 AND 51-20-4.