What was found
During H ck in Atl, The rear spar, lower cap aft flange at approx. at approximately sta xrs 80 was found to be corroded and cracked. The damage was blended out and protected against corrosion. Material 2024-t3511 EA 99-185232
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
During H ck in Atl, The rear spar, lower cap aft flange at approx. at approximately sta xrs 80 was found to be corroded and cracked. The damage was blended out and protected against corrosion. Material 2024-t3511 EA 99-185232