What was found
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .125 INCH CRACK AFT ENTRY DOOR LOWER HINGE CUTOUT, LOWER FORWARD EDGE OF FUSELAGE SKIN. INSTALLED DOUBLER AND TRIPLER, REPAIRED PER SRM 53-30-3 FIG 34. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .125 INCH CRACK AFT ENTRY DOOR LOWER HINGE CUTOUT, LOWER FORWARD EDGE OF FUSELAGE SKIN. INSTALLED DOUBLER AND TRIPLER, REPAIRED PER SRM 53-30-3 FIG 34. (M)