1/4/2022 | 7616999008 | SUPPORT: 1.P/N BACN10GH3-10 = 3 PCS. 2.P/N BACN10GH3-8 = 19 PCS 3.P/N BACN10GH3-2 = 1 PC MADE FROM ALUMINUM ALLOY, INTENDED FOR FASTENING PARTS AT A CERTAIN DISTANCE TO THE SUPPORTING STRUCTURAL ELEMENTS. | 0.14 | 378.6 | United States of America | MOSCOW RUSSIA | PJSC SCIENTIFIC AND PRODUCTION CORPORATION IRKUT |
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 |
1/22/2022 | 7616999008 | GASKET H/N BACS40R010Y033F. MADE FROM ALUMINUM ALLOYS, METHOD OF STAMPING. RECTANGULAR FORM. IT IS USED FOR FASTENING ELEMENTS IN THE FLIGHT CONTROLS SYSTEM OF THE ACFT. FOR REPAIR AND MAINTENANCE OF CIVIL PASSENGER | 0.09 | 261.33 | United States of America | HAYALIA GARDENS | PJSC AIRLINE UTair |
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 |
1/1/2022 | 7616999008 | JOINT ASSEMBLY B/N 65-50821-1029, ALUMINUM ALLOY DURALUMINUM-ALUMINUM AL (BASE) WITH COPPER CU (1.4-1.3%), MAGNESIUM MG (0.4-2.8%) AND MANGANESE MN (0,2-1%), PROCESSING METHOD - TURNING WITH GRINDING, PAINTED, WITH FASTENING ELEMENTS | 0.07 | 15280 | United States of America | GOODIER | PJSC AIRLINE UTair |
1/5/2022 | 7616999008 | ANGLE BRACKET FASTENING GASKET PANEL FLAPS BOEING 737 CIVIL AVIATION: | 0.19 | 1680.7 | United States of America | SEATTLE AIRPORT USA | S 7 ENGINEERING LLC |
1/7/2022 | 7616999008 | RETAINING PLATE FOR FASTENING THE SEAL OF THE TOP PART OF THE OUTER FLAPS OF THE WING PLANE OF PASSENGER ACFT B737. | 0.01 | 1146.9 | United States of America | MIAMI | S 7 ENGINEERING LLC |
1/21/2022 | 7616999008 | FITTING P/N A704263-101 = 2 PCS MADE FROM ALUMINUM ALLOY. INTENDED FOR FASTENING THE EQUIPMENT TO AIRCRAFT FRAMES, STRINGERS AND SPARS. MANUFACTURING METHOD - MILLING. FITTING FOR FASTENING ELEMENTS (PARTS) OF INTERIOR SYSTEM PASSENGER | 0.06 | 1255.4 | United States of America | EVERETT | PJSC SCIENTIFIC AND PRODUCTION CORPORATION IRKUT |
1/21/2022 | 7616999008 | HANDRAIL P/N A704123-101 = 3 pcs. FITTING FOR FASTENING CEILING PANELS. MADE FROM ALUMINUM ALLOY. INTENDED FOR FASTENING THE EQUIPMENT TO AIRCRAFT FRAMES, STRINGERS AND SPARS. MANUFACTURING METHOD - MILLING. ELEMENTS (PARTS) OF SYSTEMS | 0.09 | 984.32 | United States of America | EVERETT | PJSC SCIENTIFIC AND PRODUCTION CORPORATION IRKUT |
1/31/2022 | 7616999008 | GUIDE ASSEMBLY WITH ANCHOR NUTS, FASTENING THE PULL-OUT TABLE OF THE KITCHEN UNIT OF THE PASSENGER AC HA EMBRAER 170/175. MATERIAL - ALUMINUM ALLOY (90% ALUMINUM, 10% ADDITIVES. | 0.14 | 239.57 | United States of America | MITRY MORY | PJSC AIRLINE SIBERIA |