What was found
SMALL CRACK AFT FUSELAGE INTERNAL LT CANTED FRAME STA 1200.019. INSTALLED REPAIR 15" X 2" AS REQ 51-70-11 MATERIAL USED 7075.0 .063 HEAT TREATMENT TO 7075 T6 .063 AS PER SRM 51-32.01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
SMALL CRACK AFT FUSELAGE INTERNAL LT CANTED FRAME STA 1200.019. INSTALLED REPAIR 15" X 2" AS REQ 51-70-11 MATERIAL USED 7075.0 .063 HEAT TREATMENT TO 7075 T6 .063 AS PER SRM 51-32.01.