What was found
ROA - DURING CX-1 CHECK, FOUND .5 INCH CRACK ON FUSELAGE SKIN AT AFT ENTRY CUT OUT, LOWER HINGE CUT OUT. INSTALLED REPAIR DOUBLER PER SRM 53-30-3 FIGURE 34. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
ROA - DURING CX-1 CHECK, FOUND .5 INCH CRACK ON FUSELAGE SKIN AT AFT ENTRY CUT OUT, LOWER HINGE CUT OUT. INSTALLED REPAIR DOUBLER PER SRM 53-30-3 FIGURE 34. (M)