What was found
HOU - INSPECTION FOUND A .25 INCH CRACK IN FUSELAGE SKIN AT STA 1087, LONGERON 1L. THE CRACKED AREA WAS CUT OUT AND A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-04, FIGURE 27. (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 STA 1087, LONGERON 1L. THE CRACKED AREA WAS CUT OUT AND A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-04, FIGURE 27. (X)