1/26/2022 | 8481409009 | SAFETY GROUP, PRODUCT MATERIAL IS BRASS, CONSISTS OF A PRESSURE CHAMBER IN THE FORM OF AUTOMATIC AIR BLEED FITTING WITH AUTO-CLOSING MANOMETER WITH AUTO-CLOSING, INSULATION, WITH INNER THREAD RP 1, MEMBRANE FUSE | 235 | 3328.78 | China | NINGBO CHINA | TD SANTEKHURAL LLC |
1/3/2022 | 7318290008 | PIN WITHOUT THREAD OF THE HINGE HINGE OF THE TECHNOLOGICAL DOOR OF THE FUSELAGE CENTER-SECTION FAIRING OF THE EMBRAER 170 CIVIL AVIATION PASSENGER ACFT: | 0.02 | 38.62 | Brazil | MITRY MORY | S 7 ENGINEERING LLC |
1/3/2022 | 7318290008 | AXIS WITHOUT A THREAD OF THE HINGE HINGE OF THE HINGE OF ACCESS TO THE HYDRAULIC SYSTEM UNITS OF THE FUSELAGE FAIRING E170. | 0 | 27.16 | Brazil | MITRY MORY | S 7 ENGINEERING LLC |
1/3/2022 | 7318156200 | SCREW HEX BOLT IN THE BODY OF THE THREADED PART FOR FASTENING THE HINGE OF THE TECHNICAL COMPARTMENT HATCH LOCATED IN THE CENTRAL PART OF THE EMBRAER 170/175 AC FUSELAGE. | 0 | 13.43 | France | MITRY MORY | S 7 ENGINEERING LLC |
1/1/2022 | 7318156200 | SCREW HEX BOLT IN THE BODY OF THE THREADED PART FOR FASTENING THE HINGE OF THE TECHNICAL COMPARTMENT HATCH LOCATED IN THE CENTRAL PART OF THE EMBRAER 170/175 AC FUSELAGE. DIAMETER - 6 MM. MATERIAL: CORROSION-RESISTANT STEEL. | 0.01 | 226.16 | France | MITRY MORY | S 7 ENGINEERING LLC |
1/3/2022 | 7318156200 | A BOLT WITH A FLAT HEAD AND INTERNAL HEX IN THE BODY OF THE THREADED PART, FOR FASTENING THE HINGE OF THE SERVICE COMPARTMENT HATCH, LOCATED IN THE AER FUSELAGE OF EMBRAER 170 CIVIL AVIATION ACFT: | 0.04 | 102.39 | France | MITRY MORY | S 7 ENGINEERING LLC |
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 |