| DATE | HS_CODE | Product Description | Trademark | Country | Net Weight | Statistical Cost | Place | Shipper Name | Consignee Name |
|---|
| 2017-09-01 | 8108909009 | Round head screw Phillips, MOUNTING PIPELINE CONDITIONING SYSTEMS. MATERIAL FABRICATION: TITANIUM ALLOY (90% titanium, 10% impurities). Diameter: 5MM. LOCATION: ceiling panels passenger cabin of AC V76 GA: 7 | *** | UNITED STATES | 0.2 | 82,66 | *** | ***** | ***** |
| 2017-09-05 | 8108909009 | Countersunk screw and beveled Phillips. MATERIAL - TITANIUM ALLOY (90% titanium, 10% - ADDITIVES). DOES NOT CONTAIN Drago. METALS. SERVE (EG) panel fixing fuselage skin Sun GA A319 / 320. : P / N ASNA2001V3-25 WENCOR UNKNOWN 15 | *** | UNITED STATES | 0.06 | 312,14 | *** | ***** | ***** |
| 2017-09-11 | 8108909009 | FASTENING SCREW FLOOR PANELS Cockpit sun HA A319 / A320 MATERIAL - TITANIUM ALLOY (90% - titanium, 10% - Additives CONTAINS Drago METALS.): P / N ABS0376-3-30 goods packed in dense packing with plenty PAPER SEAL TO SAVE | *** | UNITED STATES | 3.76 | 1310,27 | *** | ***** | ***** |
| 2017-09-13 | 8108909009 | PANEL B / H 143A8333-9, the titanium alloy (chemical composition: titanium-95% aluminum 2.2%, 1.3% zirconium, niobium, 0.8%, Molybdenum-0, 5%, silicon- 0.2%) MANUFACTURING METHOD: forming, with further processing, be sanded, painted, with technological ho | *** | UNITED STATES | 2.37 | 2362,12 | *** | ***** | ***** |
| 2017-09-13 | 8108903009 | PANEL B / H 146A8342-7, CONSTRUCTED FROM TITANIUM ALLOYS (CHEMICAL COMPOSITION: 87% titanium, 10% aluminum, 3% nickel) PUNCHING METHOD WITH SUBSEQUENT lathing and coloring complex forms as a profile with a drilled TECHNOLOGICAL take,: TSIs | *** | UNITED STATES | 7.76 | 8101,67 | *** | ***** | ***** |
| 2017-09-20 | 8108909009 | Capscrews Phillips from titanium, diameter 4 mm, DECORATIVE PANEL MOUNTING IN THE PASSENGER COMPARTMENT sun 737 CIVIL AVIATION: P / N BACS12ER3K5 LABELING 724-62911531 NOT MILITARY. For maintenance or REM | *** | UNITED STATES | 0.03 | 63,64 | *** | ***** | ***** |
| 2017-09-22 | 8108909009 | PANEL B / H 65-18621-5. CONSTRUCTED FROM TITANIUM ALLOY (CHEMICAL COMPOSITION: TITAN-86.5%, aluminum-8.8%, 1.8% zirconium, niobium, 1.5% molybdenum 1.2%, silicon-0.2%) , stamping method, turning and staining. Complex shapes, set to: SYSTEM | *** | UNITED STATES | 0.78 | 2459,32 | *** | ***** | ***** |
| 2017-09-22 | 8108909009 | PANEL B / H 143A8333-9 CONSTRUCTED FROM TITANIUM ALLOYS (CHEMICAL COMPOSITION: 87% titanium, 10% aluminum, 3% nickel), PROCESS FOR PRODUCING-stamping, with further processing, polishing, coloring, installed on the system on board the aircraft FUSELAGE FOR | *** | UNITED STATES | 0.8 | 941,3 | *** | ***** | ***** |
| 2017-09-22 | 8108903009 | PANEL B / H 146A8342-7, CONSTRUCTED FROM TITANIUM ALLOYS (CHEMICAL COMPOSITION: 87% titanium, 10% aluminum, 3% nickel) PUNCHING METHOD WITH SUBSEQUENT lathing and coloring complex forms as a profile with a drilled TECHNOLOGICAL take,: TSIs | *** | UNITED STATES | 2.05 | 2591,78 | *** | ***** | ***** |
| 2017-10-30 | 8108909009 | SCREW KREPLENIYA SEXUAL PANELI LUGGAGE OTSEKA Amphibious GA BOING737, MATERIAL - TITANS. ALLOY: | *** | UNITED STATES | 0.89 | 462,73 | ATLANTA | ***** | ***** |