What was found
ROA - DURING CX-5 CHECK VISUAL/EDDY CURRENT INSPECTION, FOUND 4.5 INCH CRACK, 3.25 INCH CRACK AT STRINGER 17R BS 727B FUSELAGE SKIN. INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3 PAGE 11. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
ROA - DURING CX-5 CHECK VISUAL/EDDY CURRENT INSPECTION, FOUND 4.5 INCH CRACK, 3.25 INCH CRACK AT STRINGER 17R BS 727B FUSELAGE SKIN. INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3 PAGE 11. (M)