DATE | HS_CODE | Product Description | Trademark | Country | Net Weight | Statistical Cost | Place | Shipper Name | Consignee Name |
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2017-10-05 | 8411810009 | GAS TURBINE PLANT FOR USE ON PASSENGER civil aircraft as an auxiliary power unit (APU). PROVIDE AIRCRAFT airflow and power / used, production date 27.06.1992G., Engine power | HONEYWELL | UNITED STATES | 77 | 211272,53 | CHEREPOVETS | ***** | ***** |
2017-10-05 | 8411810009 | GAS TURBINE PLANT FOR USE ON PASSENGER civil aircraft as an auxiliary power unit (APU). PROVIDE AIRCRAFT airflow and power / used, production date 27.06.1992G., Engine power | HONEYWELL | UNITED STATES | 77 | 211272,53 | CHEREPOVETS | ***** | ***** |
2017-10-09 | 8411810009 | AIR POWER PLANT, which is a single-shaft gas turbine engine at a constant speed ROTATION installed in the rear fuselage-in unsealed properly oriented APU were selected ELECTRIC POWER NOT EXCEEDING 40KW, CM. | HONEYWELL | UNITED STATES | 105.2 | 1464236,04 | PHOENIX | ***** | ***** |
2017-10-09 | 8411990098 | Part of the auxiliary single-shaft gas turbine engine power not exceeding 40 kW auxiliary power unit - Fuel JET on the perimeter of the camera body with combustion are ten fuel injectors VORTEX TIPA.ONI | HONEYWELL | UNITED STATES | 0.6 | 10690,45 | PHOENIX | ***** | ***** |
2017-10-09 | 8411810009 | AIR POWER PLANT, which is a single-shaft gas turbine engine at a constant speed ROTATION installed in the rear fuselage-in unsealed properly oriented APU were selected ELECTRIC POWER NOT EXCEEDING 40KW, CM. | HONEYWELL | UNITED STATES | 105.2 | 1464236,04 | PHOENIX | ***** | ***** |
2017-10-09 | 8411990098 | Part of the auxiliary single-shaft gas turbine engine power not exceeding 40 kW auxiliary power unit - Fuel JET on the perimeter of the camera body with combustion are ten fuel injectors VORTEX TIPA.ONI | HONEYWELL | UNITED STATES | 0.6 | 10690,45 | PHOENIX | ***** | ***** |
2017-10-17 | 8411810001 | Auxiliary power unit P / N WE3800770-3 = 3 PCS. IS single-shaft gas turbine engines 40 kW at a constant speed ROTATION installed in the rear fuselage - in unsealed COMPARTMENT MAT. AS | HONEYWELL | UNITED STATES | 315.6 | 640113,14 | PHOENIX | ***** | ***** |
2017-10-17 | 8411810001 | Auxiliary power unit P / N WE3800770-3 = 3 PCS. IS single-shaft gas turbine engines 40 kW at a constant speed ROTATION installed in the rear fuselage - in unsealed COMPARTMENT MAT. AS | HONEYWELL | UNITED STATES | 315.6 | 640113,14 | PHOENIX | ***** | ***** |
2017-10-19 | 8411910008 | REGULATOR (P / N 441921-5, S / N CUC13282) FUEL MAT FOR MAINTENANCE AND REPAIR sun A320 / 321 / 319.1 PCS. | HONEYWELL | UNITED STATES | 3.6 | 80503,24 | EKATERINBURG | ***** | ***** |
2017-10-19 | 8411910008 | REGULATOR (P / N 441921-5, S / N CUC13282) FUEL MAT FOR MAINTENANCE AND REPAIR sun A320 / 321 / 319.1 PCS. | HONEYWELL | UNITED STATES | 3.6 | 80503,24 | EKATERINBURG | ***** | ***** |