25/Oct/2017 | 8411910008 | Steel shoulder installed on fan stage basic engine for toir sun a319 / 320/321, p / n 338-002-114-0, 6 sht.upakovka paved optional packaging materials. | FRANCE | SNECMA | *** | *** | 19.80 | 4798,78 | ***** | 84 More Columns Available along with Company Name and Other Details etc. |
20/Oct/2017 | 8411910008 | The rotor disc (b / d) fan airplane turboprop with a central hole a shaft. manufactured combined method of heat-resistant steel. on the periphery of the disc has holes for fixing blades and bolt holes. p / n | UNITED STATES | GENERAL ELECTRIC | *** | *** | 25 | 13,000 | ***** |
15/Oct/2017 | 8411910008 | Part turbojet - titanium blade rotor fan motor for bc a319 / a320 civil aviation: | FRANCE | UNKNOWN, | *** | *** | 3.60 | 47413,91 | ***** |
27/Sep/2017 | 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 | KG | 26.62 | 26938,2 | ***** |
17/Sep/2017 | 8411910008 | The rotor disc (b / d) fan airplane turboprop with a central hole a shaft. manufactured combined method of heat-resistant steel. in periphery of the disc mounting holes p / n 6078t57g05 - 1 unit, s / n gee1faeg blades and on. | UNITED STATES | *** | 25 | KG | 25 | 15,000 | ***** |
13/Sep/2017 | 8411910008 | Part.№1957m10p03 shoulder, not military purpose classification code 753100, 618-42825742 labeling: p / n 1957m10p03 - titanium fan blades of aircraft engines (turbojet) sun for maintenance and (or) repair civilian passenger | UNITED STATES | *** | 0,6 | KG | 0.60 | 10506,41 | ***** |
13/Sep/2017 | 8411910008 | Part turbojet - blade titanium straightener rotor fan motor sun airbus a319 / a320 civil aviation: p / n 338-002-114-0, not military identification 421-0629 4046 intended for acceleration and povorochivaniya in | FRANCE | *** | 3,25 | KG | 3.25 | 12801,4 | ***** |
08/Sep/2017 | 8411910008 | Part turbofan and turboprop engines not military: part.№ 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 | KG | 2.28 | 59314,82 | ***** |
07/Sep/2017 | 8411910008 | Parts of the turbojet engine, not military: classification code 753900 part.№ 338-002-114-0 - titanium blades for the fan shroud flange turbofan power plants. installed on disk rotor shaft first stage compressor. slu | FRANCE | *** | 3,34 | KG | 3.34 | 46431,03 | ***** |