What was found
AFTER REMOVING RIGHT MLG FIXED BRACE FITTING ASSEMBLY, FOUND CORROSION INSIDE THE OTBD HOLE ON THE TRAPEZOIDAL PANEL. REMOVED CORROSION AND INSTALLED A BUSHING IAW SRM 57-10-02-2R, FIG 201.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AFTER REMOVING RIGHT MLG FIXED BRACE FITTING ASSEMBLY, FOUND CORROSION INSIDE THE OTBD HOLE ON THE TRAPEZOIDAL PANEL. REMOVED CORROSION AND INSTALLED A BUSHING IAW SRM 57-10-02-2R, FIG 201.