What was found
ROA - DURING 'BX' CHECK VISUAL INSPECTION, CONFIRMED WITH HFEC, FOUND .75 INCH FUSELAGE SKIN CRACK S19L, BS 760. STOP DRILLED CRACK AND INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3, FIGURE 3. (X)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
ROA - DURING 'BX' CHECK VISUAL INSPECTION, CONFIRMED WITH HFEC, FOUND .75 INCH FUSELAGE SKIN CRACK S19L, BS 760. STOP DRILLED CRACK AND INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3, FIGURE 3. (X)