22/Sep/2017 | 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 | KG | 0.80 | 941,3 | ***** | 84 More Columns Available along with Company Name and Other Details etc. |