What was found
During Hck in Atl a crack was found in the fuselage skin at the forward service door jamb, lower aft corner. the crack was trimmed out and repaired. .050" 2024-t3 clad aluminum. Repaired per EA 96-185032.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
During Hck in Atl a crack was found in the fuselage skin at the forward service door jamb, lower aft corner. the crack was trimmed out and repaired. .050" 2024-t3 clad aluminum. Repaired per EA 96-185032.