DATE | HS_CODE | Product Description | Trademark | Country | Net Weight | Statistical Cost | Place | Shipper Name | Consignee Name |
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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 | 8421990008 | The filter element CONTROL MECHANISM valve actuator load control-is a portion of the filter (filter elements) cleaning liquid flowing into the valve load control, | HONEYWELL | UNITED STATES | 0.45 | 1043,04 | 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 | ***** | ***** |
2017-10-09 | 8421990008 | The filter element CONTROL MECHANISM valve actuator load control-is a portion of the filter (filter elements) cleaning liquid flowing into the valve load control, | HONEYWELL | UNITED STATES | 0.45 | 1043,04 | 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 | ***** | ***** |
2017-10-25 | 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 type. THEY | HONEYWELL | UNITED STATES | 0.4 | 7238,15 | PHOENIX | ***** | ***** |
2017-10-25 | 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 type. THEY | HONEYWELL | UNITED STATES | 0.4 | 7238,15 | PHOENIX | ***** | ***** |