1/20/2022 | 8108909008 | H/N BOLT HL10VF5-2,HL10VF5-3 WITH FLAT HEAD AND HEX KEY HOLE IN BOLT BODY, MATERIAL: TITANIUM ALLOY (90% - TITANIUM, 10% ADDITIVES, DOES NOT CONTAIN PRECIOUS METALS. MANUFACTURING METHOD: CASTING WITH MOLDING | 0.05 | 371.39 | United States of America | FARMINGDALE NEW YORK | AVIATION TRANSPORTATION COMPANY YAMAL JSC |
1/25/2022 | 8108909008 | BOLT WITH A FLAT HEAD AND A HOLE IN THE THREADED PART UNDER THE INTERNAL HEX HEX, FASTENING THE STRENGTH SET OF THE STRUCTURE OF THE FUSELAGE OF THE PASSENGER AC GA BOEING767. TO BE USED ACCORDING TO THE TECHNOLOGICAL INSTRUCTIONS OF THE SRM STRUCTURAL REPAIR MANUAL. | 0.02 | 44.44 | United States of America | FOREST PARK GEORGIA USA | S 7 ENGINEERING LLC |
1/25/2022 | 8108909008 | BOLT WITH A FLAT HEAD AND A HOLE IN THE THREADED PART UNDER THE INTERNAL HEX HEX, FASTENING THE STRENGTH SET OF THE STRUCTURE OF THE FUSELAGE OF THE PASSENGER AC GA BOEING767. TO BE USED ACCORDING TO THE TECHNOLOGICAL INSTRUCTIONS OF THE SRM STRUCTURAL REPAIR MANUAL. | 0.01 | 34.8 | United States of America | FOREST PARK GEORGIA USA | 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 |