What was found
DURING ROUTINE C-CHECK INSP, FOUND ANGLE AT STA 520 STRINGER 16R CRACKED. FABRICATED REPAIR ANGLE, ALODINED, PRIMED, AND INSTALLED IAW SRM 51-10-2, 51-40-3 FIG 1, 53-10-2 FIG 3.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING ROUTINE C-CHECK INSP, FOUND ANGLE AT STA 520 STRINGER 16R CRACKED. FABRICATED REPAIR ANGLE, ALODINED, PRIMED, AND INSTALLED IAW SRM 51-10-2, 51-40-3 FIG 1, 53-10-2 FIG 3.