What was found
LEFT STAB CORRODED: CENTER SECTION, REAR SPAR UPPER FWD, ATTACH CLEVIS HAS CORROSION. REMOVED BUSHING, SPOT FACED & REAMED LUG TO REMOVED CORROSION. ROTO PEENED. FABRICATED OVERSIZE BUSHING, FPI AND INSTALLED.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LEFT STAB CORRODED: CENTER SECTION, REAR SPAR UPPER FWD, ATTACH CLEVIS HAS CORROSION. REMOVED BUSHING, SPOT FACED & REAMED LUG TO REMOVED CORROSION. ROTO PEENED. FABRICATED OVERSIZE BUSHING, FPI AND INSTALLED.