What was found
DURING SCHDULED ROUTINE STRUCTURAL INSP DISCOVERED CARGO DOOR FRAME CRACKED APPROX 2.0 INCHES AT TOP FORWARD AREA OF FRAME BETWEEN FS 456 AND FS 468.25. STOP DRILLED ENDS OF CRACK AND INSTALLED 10.0 INCH REPAIR DOUBLER.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING SCHDULED ROUTINE STRUCTURAL INSP DISCOVERED CARGO DOOR FRAME CRACKED APPROX 2.0 INCHES AT TOP FORWARD AREA OF FRAME BETWEEN FS 456 AND FS 468.25. STOP DRILLED ENDS OF CRACK AND INSTALLED 10.0 INCH REPAIR DOUBLER.