What was found
AFT FUSELAGE SKIN, CRACK AT IB AFT CORNER RT ACCESS PANEL 3903. ROUTED OUT CRACK AND INSTALLED DOUBLER PER MM 53-30-0 PG 801-803.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AFT FUSELAGE SKIN, CRACK AT IB AFT CORNER RT ACCESS PANEL 3903. ROUTED OUT CRACK AND INSTALLED DOUBLER PER MM 53-30-0 PG 801-803.