As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION FOUND TWO INCH CRACKS AT THE EDGES OF THREE LIGHTENING HOLES IN C-2 DOOR INNER SKIN OVER CENTER BALANCE SPRINGS. A 1" CRACK WAS FOUND AT THE EDGE OF A LIGHTENING HOLE IN C-2 DOOR INNER SKIN AT PULLEY ACCESS PANEL. REPAIR DOUBLERS WERE INSTALLED IAW ECRA 5230-01651 AND 5230-01652.