What was found
IAH - INSPECTION FOUND A 1.5 INCH CRACK ON FUSELAGE SKIN ADJACENT TO THE LEFT AFT ATTACH ANGLE AT DORSAL FIN AREA. THE FUSELAGE SKIN WAS REPAIRED PER SRM 53-04, FIGURE 27. (X)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
IAH - INSPECTION FOUND A 1.5 INCH CRACK ON FUSELAGE SKIN ADJACENT TO THE LEFT AFT ATTACH ANGLE AT DORSAL FIN AREA. THE FUSELAGE SKIN WAS REPAIRED PER SRM 53-04, FIGURE 27. (X)