What was found
ROA - DURING 'CX-1' CHECK VISUAL INSPECTION, FOUND 1.75 INCH CRACK BS 380 BETWEEN BL '0' AND STRINGER 28 RIGHT FUSELAGE SKIN. INSTALLED DOUBLER, REPAIR PER TR 53-30-04. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
ROA - DURING 'CX-1' CHECK VISUAL INSPECTION, FOUND 1.75 INCH CRACK BS 380 BETWEEN BL '0' AND STRINGER 28 RIGHT FUSELAGE SKIN. INSTALLED DOUBLER, REPAIR PER TR 53-30-04. (M)