28/Oct/2017 | 8411810009 | Gas turbines, power not exceeding 5, 000 kw, not for military purposes.: | *** | UNKNOWN | 1 | PC | 337.80 | 298352,37 | ***** | 84 More Columns Available along with Company Name and Other Details etc. |
27/Oct/2017 | 8411810009 | Auxiliary power unit (turbine engine) part.№3800702-1 not military purpose classification code 753000: | *** | UNKNOWN | 1 | PC | 181 | 350,000 | ***** |
26/Oct/2017 | 8411810009 | Gas turbines with capacity of no more than 5000 kw for maintenance civil passenger aircraft in order to maintain their summer fitness. installed on a321 sun, tail number vp-brd | *** | UTS. | 1 | PC | 163.70 | 652576,7 | ***** |
24/Oct/2017 | 8411810009 | Auxiliary power units (b / u). it is a gas turbine of 30 kw. consists of-stage compressor, combustion chamber and box drive units. installed in tail bay technical aircraft fuselage. | *** | "ALLIEDSIGNAL INC | 1 | PC | 80 | 60,000 | ***** |
23/Oct/2017 | 8411810009 | Auxiliary power units. party. № 3800702-1, malfunction, remove from civil passenger aircraft boeing 737, overboard. № vq-boy, : | *** | ABSENT | 1 | PC | 182 | 850,600 | ***** |
20/Oct/2017 | 8411810009 | A gas turbine engine power 1103 kw: tb2-117ag turboshaft engine - 2 pcs, head.. № c91111157, s94101235. it is the main engine for grazhdanskogo mi-8 helicopter. | *** | Not labeled, RUSSIA | 2 | PC | 674 | 218,000 | ***** |
19/Oct/2017 | 8411810009 | Gas turbine op16-3a, serial № 2007-11-033 with gearbox marks zf, included in the gas turbine power (gteb) №5 on tes facilities in sochi, s. estosadok forming part of generating gas turbine unit opra dtg-one /8 | *** | OPRA TURBINES | 1 | PC | 1,670 | 110452,71 | ***** |
17/Oct/2017 | 8411810009 | Auxiliary power unit (apu) b / n 3800488-3, d / i, which is a gas turbine engine, engine power 115kw, is designed to start the main engines, provided by the onboard aircraft systems compressed air and electricity | *** | HONEYWELL | 1 | PC | 72.80 | 20,000 | ***** |
17/Oct/2017 | 8411810009 | Turbine engine ai-9v number 7080923900181, 2009g.v, b / u:. single-shaft, power 70kw, is designed to air launch turboprop engines, the development of alternating current for the onboard network, after restoration, the continued airworthiness of the gra | *** | *** | 1 | PC | 70 | 21020,88 | ***** |
13/Oct/2017 | 8411810009 | Auxiliary power units (gas turbine engines), power 202 horsepower or 149 kw. it is used to generate electricity, run basic engines, pressurize the hydraulic system and air conditioning in | *** | UNKNOWN | 1 | PC | 360 | 1,500,000 | ***** |