What was found
A 1.25 INCH CRACK ON FUSELAGE SKIN AT BS 727D + 17" - 18", S23R. INSTALLED DOUBLER REPAIR IAW SRM 53-00-01 REPAIR 3 FIG 201.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
A 1.25 INCH CRACK ON FUSELAGE SKIN AT BS 727D + 17" - 18", S23R. INSTALLED DOUBLER REPAIR IAW SRM 53-00-01 REPAIR 3 FIG 201.