What was found
A 1.125" CRACK ON FUSELAGE SKIN AT BS 1088 (AFT JACK PAD), S24R-S25R. INSTALLED DOUBLER REPAIR IAW SRM 53-80-01, REPAIR 04, FIG 201.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
A 1.125" CRACK ON FUSELAGE SKIN AT BS 1088 (AFT JACK PAD), S24R-S25R. INSTALLED DOUBLER REPAIR IAW SRM 53-80-01, REPAIR 04, FIG 201.