DATE | HS_CODE | Product Description | Trademark | Country | Net Weight | Statistical Cost | Place | Shipper Name | Consignee Name |
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2017-10-17 | 8481808508 | CONTROL VALVE gap between the stator and rotor in the low-pressure turbine, remove from commercial aircraft "AIRBUS A319". INTENDED FOR FEED THE NECESSARY AMOUNT OF COLD AIR CONTROL SYSTEM blade clearance | ABSENT | *** | 2.4 | 16622,49 | HAMBURG | ***** | ***** |
2017-10-17 | 8481201009 | Hydroallocators SYSTEM TURNING nose landing gear, removed from the commercial aircraft "AIRBUS A320". Designed to control the flow of hydraulic fluid supplied to the piston chamber CYLINDER DUAL nose gear | ABSENT | *** | 6 | 17683,5 | HAMBURG | ***** | ***** |
2017-10-17 | 8481808508 | CONTROL VALVE gap between the stator and rotor in the low-pressure turbine, remove from commercial aircraft "AIRBUS A319". INTENDED FOR FEED THE NECESSARY AMOUNT OF COLD AIR CONTROL SYSTEM blade clearance | ABSENT | *** | 2.4 | 16622,49 | HAMBURG | ***** | ***** |
2017-10-17 | 8481201009 | Hydroallocators SYSTEM TURNING nose landing gear, removed from the commercial aircraft "AIRBUS A320". Designed to control the flow of hydraulic fluid supplied to the piston chamber CYLINDER DUAL nose gear | ABSENT | *** | 6 | 17683,5 | HAMBURG | ***** | ***** |
2017-10-23 | 8471500000 | PART A BC-319 CIVIL AVIATION BORT.â„– VQ-BBD: CONTROL UNIT elevator and aileron, DWG. Number 3945128215 SERIAL SERIAL â„– ELACVB016866, is responsible for managing the elevators and ailerons. Each aircraft has two BLOKA.BLOK ALWAYS CI | Trademarks are not marked | *** | 5.86 | 104607,09 | HAMBURG | ***** | ***** |
2017-10-23 | 8471500000 | PART A BC-319 CIVIL AVIATION BORT.â„– VQ-BBD: CONTROL UNIT elevator and aileron, DWG. Number 3945128215 SERIAL SERIAL â„– ELACVB016866, is responsible for managing the elevators and ailerons. Each aircraft has two BLOKA.BLOK ALWAYS CI | Trademarks are not marked | *** | 5.86 | 104607,09 | HAMBURG | ***** | ***** |
2017-10-25 | 8483405900 | Hydromechanical transmission to adjust the output SPEED GENERATOR. It CONSISTS OF TWO HYDRAULIC POSITIVE Discrete axial piston units and Axial Mechanical TRANSMISSION DIFFERENTIAL that performs | UNKNOWN | *** | 33.18 | 97433,97 | HAMBURG | ***** | ***** |
2017-10-25 | 8483405900 | Hydromechanical transmission to adjust the output SPEED GENERATOR. It CONSISTS OF TWO HYDRAULIC POSITIVE Discrete axial piston units and Axial Mechanical TRANSMISSION DIFFERENTIAL that performs | UNKNOWN | *** | 33.18 | 97433,97 | HAMBURG | ***** | ***** |
2017-10-30 | 8481808508 | OF CIVIL AVIATION AIRCRAFT (AIRBUS A319 / A320): CONTROL VALVE gap between the stator and rotor in the low-pressure turbine, is designed to supply the required amount of cool air into the system CONTROL blade clearance K | ABSENT | *** | 2.4 | 16392,65 | HAMBURG | ***** | ***** |
2017-10-30 | 8481808508 | OF CIVIL AVIATION AIRCRAFT (AIRBUS A319 / A320): CONTROL VALVE gap between the stator and rotor in the low-pressure turbine, is designed to supply the required amount of cool air into the system CONTROL blade clearance K | ABSENT | *** | 2.4 | 16392,65 | HAMBURG | ***** | ***** |