1/28/2022 | 7318220008 | FLAT WASHER, NON-SPLIT, NON-LOCKING, FOR THE FASTENING ASSEMBLY OF A STRINGER TO THE CROSS BEAM OF THE POWER STRUCTURE OF THE FUSELAGE OF THE PASSENGER AC GA EMBRAER 170/175. | 0.01 | 19.83 | United States of America | MIAMI | S 7 ENGINEERING LLC |
1/28/2022 | 7616100000 | SOLID HEAD RIVET FOR FASTENING ANCHOR NUT INSTALLATION ATC ANTENNA LOWER FUSELAGE AIRCRAFT HA E170. | 0.01 | 25.24 | United States of America | MIAMI | S 7 ENGINEERING LLC |
1/24/2022 | 8807300000 | RESCUE SLIDE (CHUTTER) (USED, RESTORED) IS USED FOR EMERGENCY LEAVING OF THE AIRCRAFT BY PASSENGERS AND MEMBERS OF THE AIRCRAFT CREW. MADE OF NYLON FABRIC COATED WITH POLYURETHANE. INSTALLED IN THE CENTRAL PART OF THE PASSENGER FUSELAGE | 90 | 58176 | United States of America | KANSAS CITY AIRPORT | AIRLINE ROYAL FLIGHT JSC |
1/24/2022 | 8308200000 | A NICKEL BULL RIVET IS USED FOR FASTENING THE BRACKET TO THE REAR, TOP PART OF THE BELL 407 CIVIL HELICOPTER FUSELAGE, WHICH IS INTENDED FOR FASTENING THE OIL COOLER COMPARTMENT HOOD AND TAIL GEAR DRIVE SHAFT FAIRING: ART. | 0.17 | 289.19 | United States of America | BADHOEVEDORP | AOKAZAN AIRLINE |
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 |
1/24/2022 | 7326909409 | THE ROD END IS A PART OF A DAMPERING DEVICE THAT REDUCES VIBRATIONS THAT ARE TRANSMITTED TO THE POWER PART OF THE HELICOPTER FUSELAGE DURING THE ROTATION OF THE ROOT. | 0.1 | 2174.67 | United States of America | BADHOEVEDORP | AOKAZAN AIRLINE |
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 |
1/13/2022 | 7318162000 | STEEL NUTS TURNED FROM RODS WITH INNER DIAMETER 4 MM, WITH THREAD, WITHOUT ADDITIONAL STRUCTURAL ELEMENTS, FOR FASTENING AIRCRAFT PARTS (FUSELAGE, WINGS, TAIL, ENGINE) USING BOLT CONNECTIONS, ZAP. PARTS | 0.04 | 362.43 | United States of America | TEXAS | SIMAVIA LLC |
1/27/2022 | 7318290008 | PINS MADE FROM STAINLESS STEEL. QUICK COUPLING WITHOUT A THREAD, WITH A ROUND HEAD AND A STRAIGHT (FLAT) SLOT. INTENDED FOR FIXING QUICK-RELEASE PANELS (FUSELAGE FAIRINGS) ON THE AIRCRAFT. WITHOUT ADDITIONAL ELEMENTS | 0.47 | 491.12 | United States of America | MONTEREY PARK | PJSC SCIENTIFIC AND PRODUCTION CORPORATION IRKUT |