1/15/2022 | 8108909008 | SCREW H/H BACS12GP3L15, MADE OF TITANIUM ALLOYS (CHEMICAL COMPOSITION: TITANIUM-88%, ALUMINUM-6.75%, VANADIUM-4.5%). HEADED, CROSS SLOTTED, 5MM DIAMETER THREADED, WITH POINTED END. ADDITIONAL STRUCTURAL ELEMENTS NOT AVAILABLE | 1.07 | 1272.49 | United States of America | HAMBURG AIRPORT GERMANY | PJSC AIRLINE UTair |
1/23/2022 | 8108909008 | SCREW H/H BACS12FA3K10, MADE OF TITANIUM ALLOYS (CHEMICAL COMPOSITION - TITANIUM-95%, ALUMINUM-2.2%, ZIRCONIUM-1.3%, NIOBIUM-0.8%, MOLYBDENUM-0.5%, SILICON-0 ,2%, ) THREADED, NOMINAL OD 4 MM, CROSS HEAD | 2.21 | 1177.8 | United States of America | PICHTRY CITY ATLANTA USA | PJSC AIRLINE UTair |
1/30/2022 | 8108909008 | SCREW HEAD BOLT. THE END OF THE THREADED PART HAS AN INTERNAL HEXAGONAL SLOT. IS A FASTENING ELEMENT OF THE WING OF A PASSENGER ACFT GA B737. MATERIAL - TITANIUM ALLOY (90% TITANIUM, 10% ADDITIVES). DIAMETER - 6 MM. | 0.2 | 339.25 | United States of America | FOREST PARK GEORGIA USA | S 7 ENGINEERING LLC |
1/22/2022 | 8108909008 | SCREW HEAD BOLT AND SLOT IN THE THREADED PART UNDER INTERNAL HEX, FASTENING THE LOWER PANEL OF THE WING OF A PASSENGER ACFT BOEING737. MATERIAL: TITANIUM ALLOY (90% TITANIUM, 10% ADDITIVES). MANUFACTURING METHOD: PRESSING, THREADING. | 0.02 | 200.33 | United States of America | FORDINGBRIDGE HAMPSHIRE | S 7 ENGINEERING LLC |
1/26/2022 | 8108909008 | SCREW H/N BACS12ER06K8, THREADED, TITANIUM ALLOY (CHEMICAL COMPOSITION: TITANIUM-88%, ALUMINUM-7.5%, VANADIUM-4.5%), PHILLIOS SPOT HEAD, NO ADDITIONAL CONSTRUCTION COMPONENTS, USE FOR FASTENING ELEMENTS IN C | 0 | 31.69 | United States of America | FOREST PARK GEORGIA USA | PJSC AIRLINE UTair |
1/12/2022 | 8108909008 | SCREW H/N BACS12ER06K8, THREADED, TITANIUM ALLOY (CHEMICAL COMPOSITION: TITANIUM-88%, ALUMINUM-7.5%, VANADIUM-4.5%), PHILLIOS SPOT HEAD, NO ADDITIONAL CONSTRUCTION COMPONENTS, USE FOR FASTENING ELEMENTS IN C | 0.01 | 129.1 | United States of America | HOUNSLOW | PJSC AIRLINE UTair |
1/25/2022 | 8108909008 | SCREW HEAD BOLT AND A HOLE IN THE THREADED PART UNDER THE INTERNAL HEXAGON, FASTENING THE POWER BEAM ASSEMBLY OF THE HINGE OF THE HINGE OF THE ENGINE REVERSE BOEING 737. MATERIAL - TITANIUM ALLOY (90% - TITANIUM, 10% ADDITIVES). DIAMETER - 6 MM. WAY | 0.03 | 31.08 | United States of America | HESTON | S 7 ENGINEERING LLC |
1/25/2022 | 8108909008 | SCREW HEAD BOLT AND A HOLE IN THE THREADED PART UNDER THE INTERNAL HEXAGON, FASTENING THE POWER BEAM ASSEMBLY OF THE HINGE OF THE HINGE OF THE ENGINE REVERSE BOEING 737. MATERIAL - TITANIUM ALLOY (90% - TITANIUM, 10% ADDITIVES). DIAMETER - 6 MM. WAY | 0.14 | 289.2 | United States of America | HESTON | S 7 ENGINEERING LLC |
1/25/2022 | 8108909008 | SCREW HEAD BOLT AND HOLE IN THE THREADED PART UNDER INTERNAL HEXAGON, FASTENING THE STRENGTH SET OF THE FUSELAGE STRUCTURE OF BOEING 767 ACFT. MATERIAL - TITANIUM ALLOY (90% - TITANIUM, 10% ADDITIVES). DIAMETER - 6 MM. MANUFACTURING METHOD - PRESSING, | 0.01 | 36.62 | United States of America | HESTON | S 7 ENGINEERING LLC |