1/28/2022 | 7506200009 | NICKEL ALLOY PLATE, NOT FOR AIRCRAFT ENGINES, GROSS WEIGHT WITH PALLET 420.00 KG : | 390 | 27217.9 | United States of America | RZESZOW | CJSC KHAMILTON STANDARD SCIENCE |
1/21/2022 | 8708939009 | NEW DAMPER CLUTCH FROM NON-ALLOYED NON-CORROSION-RESISTANT STEEL. IT IS DESIGNED FOR DAMPING ENGINE RPM OSCILLATIONS, AS WELL AS CONNECTING THE ENGINE FLYWHEEL TO THE GEARBOX. CONSISTS OF A DRIVE PLATE WHICH IS ATTACHED TO THE FLYWHEEL | 1392 | 40558.8 | United States of America | ROCHESTER HILLS | KZ ROSTSELMASH ON ORDER OF LLC MITAS LLC |
1/4/2022 | 7616999008 | ALUMINUM ALLOY PLATE (SPACE): A336411-161 = 1 PC. PLATE WITH A HOLE IN THE CENTER IS INTENDED FOR FASTENING THE WATER SUPPLY SYSTEM PIPE CLAMP. IZGO | 0 | 5.6 | United States of America | MOSCOW RUSSIA | PJSC SCIENTIFIC AND PRODUCTION CORPORATION IRKUT |
1/4/2022 | 8108909008 | PLATE H/N 143A8333-8, MADE OF TITANIUM ALLOYS (CHEMICAL COMPOSITION: 87% TITANIUM, 10% ALUMINUM, 3% NICKEL) TECHNICAL | 2.29 | 1602.32 | United States of America | SUNRISE | PJSC AIRLINE UTair |
1/5/2022 | 8481900000 | PART OF THE WEDGE GATE VALVE TYPE B & DB - THE GUIDE PLATE OF THE SHUT-OFF WEDGE (GATE) MADE OF ALLOYED STEEL, PART. NUMBER 10179998-001 / 717909 | 0.34 | 34.22 | United States of America | Unknown | EXXON NEFTEGAZ LIMITED |
1/26/2022 | 8310000000 | MARKER H/N BAC27DWG26, REPRESENTS AN INFORMATION PLATE. MADE FROM ALUMINUM ALLOY, METHOD OF TURNING. SELF-ADHESIVE, RECTANGULAR SHAPED. HAS AN INFORMATION SIGN IN ENGLISH.YAZ. INSTALLED IN THE WING SYSTEM OF THE ACFT. FOR R | 0 | 32.86 | United States of America | HOUNSLOW | PJSC AIRLINE UTair |
1/1/2022 | 7616100000 | RIVET WITH SOLID HEAD, SOLID, FOR FASTENING OF ANTENNA PLATE OF AUTOMATIC RADIO COMPASS OF PASSENGER AIRCRAFT E170/175. MATERIAL - ALUMINUM ALLOY (90% - ALUMINUM, 10% - DOES NOT CONTAIN PRECIOUS METALS). DIAMETER - 4 MM. | 0 | 21.92 | United States of America | MITRY MORY | S 7 ENGINEERING LLC |
1/5/2022 | 7616999008 | VULCANIZED RUBBER DAMPER PAD WITH ALUMINUM ALLOY MOUNTING PLATE AND INTERNAL THREADED BUSHING FOR BOEING 737 CIVIL AVIATION PILOT CABIN CEILING PANELS FASTENING PURPOSE - | 0.04 | 95.95 | United States of America | SITAK | S 7 ENGINEERING LLC |
1/4/2022 | 8310000000 | PLATE H/N BAC27DLG0145, FROM ALUMINUM ALLOYS (DURALUM, CHEMICAL COMPOSITION OF THE MATERIAL: ALUMINUM 93.2%, COPPER 4.5%, MAGNESIUM 1.6%, MANGANESE 0.7%), MANUFACTURING METHOD: STAMPING, WITH FURTHER PROCESSING - GRINDING, WITHOUT BACKING, SELF-ADHESIVE, THICKNESS 0, | 0.01 | 96.69 | United States of America | GOODIER | PJSC AIRLINE UTair |
1/11/2022 | 7606910000 | PLATES, SHEETS, STRIPS OR TAPE, OF NON-ALLOYED ALUMINUM, MORE THAN 0.2 MM THICKNESS: | 34.4 | 2012.95 | United States of America | MOSCOW RUSSIA | 3M RUSSIA JSC |