What was found
INSPECTION FOUND A 1.5 INCH CRACK BETWEEN FORWARD TWO LIGHTENING HOLES OF THE BOTTOM ROW OF MAIN CABIN DOOR STIFFENER. A NEW STIFFENER AND FILLER WERE 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 BETWEEN FORWARD TWO LIGHTENING HOLES OF THE BOTTOM ROW OF MAIN CABIN DOOR STIFFENER. A NEW STIFFENER AND FILLER WERE INSTALLED IAW SRM 51-30-2.