1/5/2022 | 8108909008 | BOLT WITH A FLAT HEAD AND INTERNAL HEXAGONAL SLOT IN THE THREADED PART. IT IS USED FOR FASTENING THE FUSELAGE ELEMENTS OF THE BOEING737 PASSENGER AIRCRAFT AT PERFORMING REPAIR PROCEDURES OF THE POWER KIT. MATERIAL: TITANIUM ALLOY (90%-TITANIUM, 10 | 0.04 | 69.88 | United States of America | HESTON | S 7 ENGINEERING LLC |
1/5/2022 | 8108909008 | BOLT WITH A FLAT HEAD AND INTERNAL HEXAGONAL SLOT IN THE THREADED PART. USED FOR FASTENING THE FUSELAGE ELEMENTS OF THE PASSENGER AIRCRAFT BOEING737 WHEN PERFORMING REPAIR PROCEDURES OF THE POWER KIT.MATERIAL: TITANIUM ALLOY (90%-TITANIUM, 10% | 0.04 | 21.36 | United States of America | HESTON | S 7 ENGINEERING LLC |
1/30/2022 | 8108909008 | THE SCREW IS MADE OF TITANIUM ALLOY (TITANIUM - 90%, ALUMINUM - 6%, VANADIUM - 4%), HAS A CROSS-SHAPED ROUND HEAD, NOMINAL THREAD DIAMETER 5 MM. WORKS FOR CUTTING, STRENGTH 630 MPA. DESIGNED FOR FASTENING FUSELAGE PANELS | 0.25 | 333.42 | United States of America | LONDON | NORDAVIA REGIONAL AIRLINES JSC |
1/18/2022 | 8108909008 | SCREW BOLT WITH HEXAGONAL HOLE IN THE BODY, FASTENING THE PANELS OF THE STRUCTURAL ELEMENTS OF THE FUSELAGE OF THE GA PASSENGER ACFT BOEING 737. THREAD DIAMETER: 5 MM. MATERIAL - TITANIUM ALLOY (90% TITANIUM; 10% IMPURITY). DOES NOT CONTAIN PRECIOUS METALS. | 0.02 | 18.16 | United States of America | PHOENIX AIRPORT | S 7 ENGINEERING LLC |
1/18/2022 | 8108909008 | SCREW BOLT WITH HEXAGONAL HOLE IN THE BODY, FASTENING THE PANELS OF THE STRUCTURAL ELEMENTS OF THE FUSELAGE OF A PASSENGER ACFT BOEING 737. THREAD DIAMETER: 6 MM. MATERIAL - TITANIUM ALLOY (90% TITANIUM; 10% IMPURITY). | 0.03 | 30.58 | United States of America | PHOENIX AIRPORT | 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. | 0.02 | 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 |