| 3/30/2024 | 84119900 | 5326692#&Fixed wing guiding hot air flow in aircraft engine turbine area made of nickel alloy, size 670Dx210H mm, (NW: 23 kg), 100% new item#&VN | XXXXXXXXXX | 3 | PCE | 182844.3 | South Korea | NA |
| 3/30/2024 | 84119900 | 5326692#&Fixed wing guiding hot air flow in aircraft engine turbine area made of nickel alloy, size 670Dx210H mm, (NW: 23 kg), 100% new item#&VN | XXXXXXXXXX | 2 | PCE | 121896.2 | South Korea | NA |
| 3/30/2024 | 84119900 | 5321065-01-KUN#&Bearing bracket for stage 1 and 1.5 of turbine compartment, made of titanium alloy, size D640 x H270, assembly detail in aircraft engine#&VN | XXXXXXXXXX | 2 | PCE | 29421.46 | USA | NA |
| 3/30/2024 | 84119900 | 5326692#&Fixed wing guiding hot air flow in aircraft engine turbine area made of nickel alloy, size 670Dx210H mm, (NW: 23 kg), 100% new item#&VN | XXXXXXXXXX | 9 | PCE | 548532.9 | South Korea | NA |
| 3/29/2024 | 84119900 | KH48923 J#&Medium pressure turbine detail made of Nickel alloy, size 100 x 70 x 50 (mm) used to ensure high temperature and pressure airflow ratio in aircraft engine turbines#&VN | XXXXXXXXXX | 80 | PCE | 71598.704 | United Kingdom | NA |
| 3/29/2024 | 84119900 | 5316965 B#&High pressure chamber turbine seal cover, made of nickel alloy, assembly detail in aircraft engine#&VN | XXXXXXXXXX | 6 | PCE | 24592.86 | South Korea | NA |
| 3/29/2024 | 84119900 | KH15635 G#&Components to install into the engine in the medium heating stage to ensure the temperature and pressure ratio in the aircraft engine turbine, size 99*56*73 mm#&VN | XXXXXXXXXX | 57 | PCE | 48022.8021 | United Kingdom | NA |
| 3/29/2024 | 84119900 | 5326692#&Fixed wing guiding hot air flow in aircraft engine turbine area made of nickel alloy, size 670Dx210H mm, (NW: 23 kg), 100% new item#&VN | XXXXXXXXXX | 5 | PCE | 304740.5 | South Korea | NA |
| 3/29/2024 | 84119900 | 5316965 B#&High pressure chamber turbine seal cover, made of nickel alloy, assembly detail in aircraft engine#&VN | XXXXXXXXXX | 2 | PCE | 8197.62 | South Korea | NA |
| 3/29/2024 | 84119900 | KH15635 G#&Components to install into the engine in the medium heating stage to ensure the temperature and pressure ratio in the aircraft engine turbine, size 99*56*73 mm#&VN | XXXXXXXXXX | 61 | PCE | 51392.8233 | United Kingdom | NA |