1/27/2022 | 7318155200 | CROSS HEAD BOLT, EMBRAER170 ACFT FUSELAGE PANEL FIXINGS. MATERIAL - CORROSION-RESISTANT STEEL, PRESSING, THREADING. DIAMETER - 8 MM | 0.06 | 91.46 | United States of America | MIAMI | S 7 ENGINEERING LLC |
1/4/2022 | 7318220008 | WASHER, NON-SPRING, STEEL, NO THREAD. IT IS USED IN ON-BOARD CONNECTION OF SPARE PARTS AND SYSTEMS OF ENGINE AND FUSELAGE OF PASSENGER HELICOPTER. ADDITIONAL STRUCTURAL ELEMENTS (GROOVES, GROOCHES, SLOTS, HOLES, NOTCHES) DO NOT HAVE. | 0.22 | 73.7 | United States of America | TORRANCE USA | AK LIGHT AIR JSC |
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 |
1/9/2022 | 8308200000 | RIVET H/H BACR15DR3-8, TUBE, MADE FROM ALUMINUM ALLOYS. EXHAUST, CONSISTS OF THE END OF THE RIVET AND A TEAR-OFF SHANK WITH A THREAD. DESIGNED FOR FIXED FASTENING OF PARTS IN THE AIR FUSELAGE SYSTEM FOR REPAIR AND MAINTENANCE | 0.01 | 204.44 | United States of America | HAMBURG AIRPORT GERMANY | PJSC AIRLINE UTair |
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 |
1/10/2022 | 7318155900 | SCREW H/N 66-22655-2, BLACK METAL (NON-CORROSION-RESISTANT STEEL), THREADED, PHILLIOS, SPOT HEAD, SHAFT DIAMETER 6 MM, FOR INSTALLATION IN AIRCRAFT FUSELAGE SYSTEM, FOR ACCESSORIES | 0.04 | 943.83 | United States of America | HOUNSLOW | PJSC AIRLINE UTair |
1/12/2022 | 7318163008 | PLATE NUT BH/H BACN10JZ3C2CDMU, FOR FASTENING FUSELAGE FRAME FRAME, MADE OF CORROSION-RESISTANT STEEL, WITH THREAD, ADDITIONAL STRUCTURAL ELEMENTS (GROOVES/ROOTS/SLOTS/HOLES/KNOCKS/LUGS) | 0.1 | 322.53 | United States of America | HOUNSLOW | PJSC AIRLINE UTair |
1/29/2022 | 7318155200 | SCREW HEAD BOLT FOR FASTENING THE PASSENGER PASSENGER ACFT FUSELAGE PANEER EMBRAER170/175. MATERIAL - CORROSION-RESISTANT STEEL, PRESSING, THREADING. DIAMETER - 8 MM. P/N: | 0.03 | 77.68 | United States of America | MUNICH 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 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 |