DATE | HS_CODE | Product Description | Trademark | Country | Net Weight | Statistical Cost | Place | Shipper Name | Consignee Name |
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2017-11-02 | 7606129209 | SHEET (HIRE) FLAT aluminum alloy. SIZE - 3660H1220 MM. .. THICKNESS 0.056 "(1.42 MM) intended for repair of sun BOING737 PANELS FUSELAGE STRUCTURE-alumina 90%, 10% ~ impurities NOT CONTAIN PRECIOUS: P / N CLAD2024T3-0056 - 1 SHEET (4.46 M2) | UNKNOWN | *** | 17.8 | 865,29 | SKHELLOYNEN | ***** | ***** |
2017-11-02 | 7604299000 | PROFILE FOR FIXING floor panel of the luggage compartment passenger aircraft HA BOING737. MATERIAL - aluminum alloy (90% aluminum, 10% ADDITIVES NOT CONTAIN Drago METALS.). : | UNKNOWN | *** | 8.7 | 629,6 | SKHELLOYNEN | ***** | ***** |
2017-11-02 | 7604299000 | PROFILE FOR FIXING floor panel of the luggage compartment passenger aircraft HA BOING737. Material - Aluminum alloy (90% aluminum, 10% of the additive, DOES NOT CONTAIN METALS Drago.): | UNKNOWN | *** | 21 | 1122,86 | SKHELLOYNEN | ***** | ***** |
2017-11-02 | 7606129209 | Aluminum sheets (rolling) FLAT aluminum alloy. SIZE - 3660H1220 MM. . THICKNESS 0.071 "(1.8mm) is designed to repair FUSELAGE PANELS Sun BOING737.SOSTAV-alumina 90%, 10% ~ impurities ARE FREE OF PRECIOUS: P / N CLAD2024T3-0071 - 4.46 M2 | UNKNOWN | *** | 22.5 | 2314,29 | SKHELLOYNEN | ***** | ***** |
2017-11-02 | 7606129209 | Aluminum sheets (rolling) FLAT aluminum alloy. SIZE - 3660H1220 MM. . THICKNESS 0.063 "(1.6 MM) intended for repair PANELS FUSELAGE sun BOING737.SOSTAV-alumina 90%, 10% ~ impurities NOT CONTAIN PRECIOUS: P / N CLAD2024T3-0063 - 1 SHEET | UNKNOWN | *** | 20 | 451,05 | SKHELLOYNEN | ***** | ***** |
2017-11-02 | 7606129209 | Aluminum sheets (rolling) FLAT aluminum alloy. SIZE - 3660H1220 MM. . THICKNESS 0.050 "(1.3 MM) intended for repair PANELS FUSELAGE sun BOING737.SOSTAV-alumina 90%, 10% ~ impurities NOT CONTAIN PRECIOUS: P / N CLAD2024T3-0050 - 1 SHEET | UNKNOWN | *** | 15.9 | 334,24 | SKHELLOYNEN | ***** | ***** |
2017-11-02 | 7606129209 | Aluminum sheets (rolling) FLAT aluminum alloy. SIZE - 3660H1220 MM. . THICKNESS 0.032 "(0.8mm) INTENDED FOR REPAIRING PANELS FUSELAGE sun BOING737.SOSTAV-alumina 90%, 10% ~ impurities NOT CONTAIN PRECIOUS: P / N CLAD2024T3-0032 - 1 SHEET | UNKNOWN | *** | 10.1 | 344,14 | SKHELLOYNEN | ***** | ***** |
2017-11-02 | 7606129209 | Aluminum sheets (rolling) FLAT aluminum alloy. SIZE - 3660H1220 MM. . THICKNESS 0.080 "(2.0mm) is designed to repair FUSELAGE PANELS Sun BOING737.SOSTAV-alumina 90%, 10% ~ impurities ARE FREE OF PRECIOUS: P / N CLAD2024T3-0080 - 1 SHEET | UNKNOWN | *** | 25.4 | 671,75 | SKHELLOYNEN | ***** | ***** |
2017-11-10 | 7604109000 | PROFILE W / H BAC1496-444-7075-T6 AMS-QQ-A-250/13, is made of unalloyed aluminum (CHEMICAL COMPOSITION MATERIAL MASS.%: 99.8% Aluminum, iron-0.15% magnesium 0 02%, manganese 0.02%, silicon-0.01%), MARK A7 complex shapes, smoothed by a non-gap | ABSENT | UNITED STATES | 2.4 | 1350,27 | SKHELLOYNEN | ***** | ***** |
2017-11-26 | 7606129209 | SHEET (RENT) FLAT aluminum alloy (90% - Aluminum, 10% -. ADDITIVES NOT CONTAIN Drago METALS.). Designed to repair FUSELAGE PANEL PASSENGER GA BC A319 / 320. : P / N BARE2024T3-0063- 4.46 M2 (SHEET 1) CLASSIFICATION 724-62319773 | UNKNOWN | UNITED STATES | 20 | 1510,51 | SKHELLOYNEN | ***** | ***** |