What was found
INSPECTION FOUND A 1.5 INCH CRACK IN AFT CABIN DOOR BEAM END FITTING AT LEFT CENTER STOP. A NEW FITTING WAS FABRICATED AND INSTALLED IAW SRM 51-30-2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 1.5 INCH CRACK IN AFT CABIN DOOR BEAM END FITTING AT LEFT CENTER STOP. A NEW FITTING WAS FABRICATED AND INSTALLED IAW SRM 51-30-2.