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 |
1/29/2022 | 7318163008 | NUT-CLIP MADE OF CORROSION-RESISTANT STEEL, WITH THREAD, USED FOR FASTENING FUSELAGE PANELS, WITHOUT GROOves, Slots, Grooves, FOR REPAIR AND MAINTENANCE OF ACFT ?319/320/321, P/N ABS0365S3-1E, 50 PCS. | 0.17 | 143.06 | France | EKATERENBURG | AIRLINE URAL AIRLINES JSC |
1/24/2022 | 7318290008 | A319/A320/A321 PASSENGER FUSELAGE FRONT ENTRY LEVER INSTALLATION BUSHING WITHOUT THREAD. MATERIAL - CORROSION-RESISTANT STEEL. | 0.01 | 771.9 | France | DUBAI | S 7 ENGINEERING LLC |
1/18/2022 | 7318290008 | STEEL FASTENERS FOR FUSELAGE PANELS ASSEMBLY, WITHOUT THREAD, WITH PLASTIC HEAD AND SPRING MECHANISM, P/N ABS0696-2-12-5, 10 PCS. WITHOUT GROOVES/DOROCHES/HOLES/NOTTS FOR REPAIR AND MAINTENANCE OF CIVIL PASSENGER AIR | 0.06 | 247.91 | France | EKATERENBURG | AIRLINE URAL AIRLINES JSC |
1/26/2022 | 7616999008 | BUSHING WITHOUT A THREAD, FASTENING THE FUSELAGE PANELS OF A321 CIVIL AVIATION PASSENGER ACFT: | 0.06 | 107.07 | France | DUBAI | S 7 ENGINEERING LLC |