As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LT MAIN LANDING GEAR DOOR INNER PAN Z-CHANNEL HAS CRACK APPROX 3.25 INCH LONG RUNNING IN THE AFT RADIUS ALONG THE AFT EDGE OF SUBJECT CHANNEL, 19.5 INCHES FROM THE AFT I/B CORNER STRAP. A REPAIR ANGLE WAS USED TO REPAIR THIS CRACK. REV A AND B REVISED THE PERMANENT REPAIR INSTRUCTIONS, PERMANENT REPAIR PER SRM 52-05 FIG 28.