What was found
HOU - INSPECTION FOUND THE AFT VENTRAL DOOR JAMB HAD A 2 INCH CRACK ON THE FORWARD SIDE OF LEFT CORNER. REPAIRED PER SRM 53-08, FIGURE 29. (X)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
HOU - INSPECTION FOUND THE AFT VENTRAL DOOR JAMB HAD A 2 INCH CRACK ON THE FORWARD SIDE OF LEFT CORNER. REPAIRED PER SRM 53-08, FIGURE 29. (X)