What was found
(AUS) LT AND RT WING SPARS P/N 68-1.4001 AND P/N 68-1.4002 CONTAINED INTERGRANULAR AND EXFOLIATION CORROSION IN THE WEBS LOCATED BEHIND THE ENGINE FIREWALLS.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
(AUS) LT AND RT WING SPARS P/N 68-1.4001 AND P/N 68-1.4002 CONTAINED INTERGRANULAR AND EXFOLIATION CORROSION IN THE WEBS LOCATED BEHIND THE ENGINE FIREWALLS.