What was found
ROA - DURING CX-1 CHECK VISUAL/EDDY CURRENT INSPECTION, FOUND .75 INCH CRACK FORWARD GALLEY DOOR CUT OUT AFT LOWER CORNER FUSELAGE SKIN (STRINGER 17 R BS 328). REMOVED CRACK AND INSTALLED DOUBLER, REPAIRED PER TR 53-10-19 REV A. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
ROA - DURING CX-1 CHECK VISUAL/EDDY CURRENT INSPECTION, FOUND .75 INCH CRACK FORWARD GALLEY DOOR CUT OUT AFT LOWER CORNER FUSELAGE SKIN (STRINGER 17 R BS 328). REMOVED CRACK AND INSTALLED DOUBLER, REPAIRED PER TR 53-10-19 REV A. (M)