What was found
HOU - INSPECTION FOUND A .25 INCH CRACK IN FUSELAGE SKIN AT FORWARD SERVICE DOOR JAMB UPPER FORWARD CORNER AND A .25 INCH CRACK AT THE LOWER AFT CORNER. DOUBLER REPAIRS WERE INSTALLED IAW SRM 53-05, FIGURE 38. (X)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
HOU - INSPECTION FOUND A .25 INCH CRACK IN FUSELAGE SKIN AT FORWARD SERVICE DOOR JAMB UPPER FORWARD CORNER AND A .25 INCH CRACK AT THE LOWER AFT CORNER. DOUBLER REPAIRS WERE INSTALLED IAW SRM 53-05, FIGURE 38. (X)