What was found
FS 280, LEFT WEB CORRODED. REMOVED CORROSION ORIGINAL THICKNESS =.035" MATERIAL REMOVED =.0045" DEEP X18"X.75". REMAINING MATERIAL THICKNESS = .0305" WITHIN ALLOWABLE LIMITS.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FS 280, LEFT WEB CORRODED. REMOVED CORROSION ORIGINAL THICKNESS =.035" MATERIAL REMOVED =.0045" DEEP X18"X.75". REMAINING MATERIAL THICKNESS = .0305" WITHIN ALLOWABLE LIMITS.