What was found
3/16 INCH CRACK IN FUSELAGE OUTER SKIN AT C2 DOOR CUTOUT UPPER AFT CORNER , FASTENER REPAIR PER SRM 53-30-3 FIG 6
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
3/16 INCH CRACK IN FUSELAGE OUTER SKIN AT C2 DOOR CUTOUT UPPER AFT CORNER , FASTENER REPAIR PER SRM 53-30-3 FIG 6