| DATE | HS_CODE | Product Description | Trademark | Country | Net Weight | Statistical Cost | Place | Shipper Name | Consignee Name |
|---|
| 2017-09-02 | 8411910008 | TITANIUM Sun BLADE MOTOR FAN EMBRAER170 Civil Aviation: P / N 4114T15P02 (P / H PROIZPODITELYA S4334-4114T15P02), LABELING 125-43608773 fan blades spinning and accelerating flow of inlet air into the engine, axially | *** | UNITED STATES | 4.2 | 21818,19 | *** | ***** | ***** |
| 2017-09-04 | 8411910008 | Parts of the turbojet engine, NOT MILITARY (CLASSIFICATION CODE 753900): PART.â„– 1765M65P07 - (ALTERNATIVE â„– 1765M65P02) (marking on the product A3460-1765M65P07) FIXED compressor blades of the turbofan engine made of titanium alloy, SERVE | *** | FRANCE | 63.8 | 275631,03 | *** | ***** | ***** |
| 2017-09-05 | 8411910001 | PART turbojet engines for the production of engines SAM146 CIVIL AVIATION: fan blades 366-000-706-0 REV. B - 137SHT. : TECT 366-000-706-0 NO REV. In 366-000-706-0 137 | *** | UNITED STATES | 305.78 | 283125 | *** | ***** | ***** |
| 2017-09-07 | 8411910008 | Parts of the turbojet engine, NOT MILITARY: CLASSIFICATION CODE 753900 PART.â„– 338-002-114-0 - titanium blades for the fan shroud flange turbofan POWER PLANTS. INSTALLED ON DISK ROTOR SHAFT first stage compressor. SLU | *** | FRANCE | 3.34 | 46431,03 | *** | ***** | ***** |
| 2017-09-07 | 8411990098 | Guide and rotor blades first, second, third and fourth stage of the gas turbine. They are part of a gas turbine. PRINCIPLE: UNDER THE INFLUENCE OF GAS FLOW BLADE generates a torque transmitted to the rotor GAS GUIDE T h | *** | GERMANY | 1345 | 23656 | *** | ***** | ***** |
| 2017-09-07 | 8411910008 | Parts of turbojets: CASTING rotor blade stage 3 a low pressure turbine (LPT) LEAP-1B for aircraft engines for civil aircraft BOEING 737 MAX, drawing NUMBER 364-023-201-9 -1279 units marking on the product "KK".: available in | *** | UNITED STATES | 112.55 | 40928 | *** | ***** | ***** |
| 2017-09-08 | 8411910008 | PART Turbofan and turboprop engines not MILITARY: PART.â„– 366-031-901-0 - COMPOSITION OF THE TWO BLADES FAN (COMPRESSOR) LOW PRESSURE GAS TURBINE ENGINE OF TITANIUM ALLOY, P / N 366-000-706-0 CC / H (AE137716, AE138370) | *** | *** | 2.28 | 59314,82 | *** | ***** | ***** |
| 2017-09-09 | 8411990019 | PART gas turbines "SGT-300" power of 7900 KW (equipment subheading 8411 82 2008), not intended for operation in explosive atmospheres blades. Loaded in a disc mounted on the rotor shaft and serves to transmit the power from the gas | *** | UNITED STATES | 0.26 | 4759,86 | *** | ***** | ***** |
| 2017-09-13 | 8411910008 | PART.â„–1957M10P03 SHOULDER, NOT MILITARY PURPOSE CLASSIFICATION CODE 753100, 618-42825742 LABELING: P / N 1957M10P03 - TITANIUM fan blades of aircraft engines (turbojet) Sun for maintenance and (or) REPAIR civilian passenger | *** | UNITED STATES | 0.6 | 10506,41 | *** | ***** | ***** |
| 2017-09-13 | 8411910008 | PART turbojet - BLADE TITANIUM straightener ROTOR FAN MOTOR Sun AIRBUS A319 / A320 CIVIL AVIATION: P / N 338-002-114-0, NOT MILITARY IDENTIFICATION 421-0629 4046 INTENDED FOR ACCELERATION AND POVOROCHIVANIYA In | *** | FRANCE | 3.25 | 12801,4 | *** | ***** | ***** |