What was found
AT C CHECK, FUSELAGE INTERIOR FRAME BODY STA 540 HAS CRACK AT STR 17R. CUT OUT DAMAGED AREA,HFEC, INSTALLED DOUBLER REPAIR PER SRM 51-40-3, 5.5 BY 6.5, N/R 3430.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AT C CHECK, FUSELAGE INTERIOR FRAME BODY STA 540 HAS CRACK AT STR 17R. CUT OUT DAMAGED AREA,HFEC, INSTALLED DOUBLER REPAIR PER SRM 51-40-3, 5.5 BY 6.5, N/R 3430.