| DATE | HS_CODE | Product Description | Trademark | Country | Net Weight | Statistical Cost | Place | Shipper Name | Consignee Name |
|---|
| 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 | *** | ***** | ***** |
| 2017-09-07 | 8411910008 | PART turbojet passenger aircraft Boeing 737-800 CIVIL AVIATION: REGULATOR FUEL, PART.NOMER 442369 DESCRIPTION: A TEAM OF FUEL UNIT hydromechanical. Assemblies are made of aluminum alloy, HAS fitting and phytin | *** | UNITED STATES | 33 | 355392,53 | *** | ***** | ***** |
| 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 | *** | ***** | ***** |
| 2017-09-11 | 8411910001 | PART Civil Aviation turbojet SAM 146: BLANK (CASTING) intermediate housing 1460600200-9L Rev. 1 - 1 PCS. DMF 20359-11 RED.V of titanium alloy TA6V (. DMD 0779-32 REV E) have the form Finished PRODUCTS: PCC STRUCTURALS INC FROM | *** | UNITED STATES | 104.87 | 74895 | *** | ***** | ***** |
| 2017-09-19 | 8411990019 | Parts of gas turbines, after cleaning and repair. For civilian use ,: fuel injector GAS TURBINE MODEL TITAN 130, used for feeding and atomization of the fuel in the combustion chamber of gas turbines. MATERIAL alloy steel. AFTER DELIVERY | *** | UNITED STATES | 234 | 117657,94 | *** | ***** | ***** |
| 2017-09-26 | 8411990098 | PARTS FOR SERVICE OF GAS TURBINES: SEGMENT DISPLAY THERMAL PROTECTION STATOR 2nd stage GAS TURBINE GT26 (POWER 280MVT) to protect the turbine stator from the heat. Material - nickel alloy gas nozzle of the second chamber combustion | *** | SWITZERLAND | 999 | 892116,71 | *** | ***** | ***** |
| 2017-09-26 | 8411990098 | PARTS FOR SERVICE OF GAS TURBINES: OUTPUT stator blades of gas turbine GT26 (POWER 280MVT). Material - nickel alloy. COMBUSTION CHAMBER EV BURNER GAS TURBINES GT26 (POWER 280MVT). GAS TURBINE ROTOR BLADE GT26 (Power | *** | SWITZERLAND | 2972.2 | 3023591,29 | *** | ***** | ***** |
| 2017-09-26 | 8411990098 | PARTS FOR SERVICE OF GAS TURBINES: PROTECTIVE COVER RING TWO COMBUSTION CHAMBER GAS TURBINES GT26 (POWER 280MVT) with a through hole on the perimeter. Material - heat-resistant chrome-nickel alloy. GE HUNGARY KFT. GE HTCZ102354R0001 1 | *** | SWITZERLAND | 215 | 9655,21 | *** | ***** | ***** |
| 2017-09-26 | 8411990098 | PARTS FOR SERVICE OF GAS TURBINES: SEGMENT DISPLAY THERMAL PROTECTION STATOR 4TH STAGE GAS TURBINE GT26 (POWER 280MVT) to protect the turbine stator from the heat. Material - nickel alloy GE POWER LTD. GE HTCT353226R0004 28 | *** | SWITZERLAND | 320 | 77621,52 | *** | ***** | ***** |
| 2017-09-27 | 8411910008 | BLADE (B / D) FAN dual circuit, an airplane turbojet. Made of titanium alloy Combined method. Mounting holes DISC ROTOR FAN airplane turbojet. APPLY TO: TURBOR | *** | *** | 26.62 | 26938,2 | *** | ***** | ***** |