What was found
ROA - DURING CX-5 CHECK VISUAL/EDDY CURRENT INSPECTION, FOUND 2 CRACKS 3.1875 INCH AND .5 INCH FORWARD GALLEY DOOR CUT OUT AFT LOWER CORNER (STRINGER 17R BS 328) FUSELAGE SKIN. INSTALLED TRIPLER, REPAIRED PER SRM 53-30-3 FIG 26. (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 2 CRACKS 3.1875 INCH AND .5 INCH FORWARD GALLEY DOOR CUT OUT AFT LOWER CORNER (STRINGER 17R BS 328) FUSELAGE SKIN. INSTALLED TRIPLER, REPAIRED PER SRM 53-30-3 FIG 26. (M)