What was found
STRINGER 41R, BETWEEN FRAME 31 - 32 HAS CORROSION. PERFORMED STINGER SPLICE REPAIR IAW SRM 53-21-13 PARA 5C FIG 203 SHEET 3. SRI53-21-13-2-003-00 TBL 204 REQUIRES INSPECTION AT 60,000C FROM ACFT 1ST FLIGHT.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
STRINGER 41R, BETWEEN FRAME 31 - 32 HAS CORROSION. PERFORMED STINGER SPLICE REPAIR IAW SRM 53-21-13 PARA 5C FIG 203 SHEET 3. SRI53-21-13-2-003-00 TBL 204 REQUIRES INSPECTION AT 60,000C FROM ACFT 1ST FLIGHT.