1/2/2022 | 7616999008 | BRACKET ASSEMBLY FOR FASTENING OF THE MANIFOLD OF THE FRONT CHASSIS TURN CONTROL SYSTEM, ON THE CEILING PANEL OF THE CHASSIS COMPARTMENT OF THE EMBRAER 170 CIVIL AVIATION PASSENGER ACFT. | 0.09 | 149.31 | Brazil | MITRI MORI | S 7 ENGINEERING LLC |
1/21/2022 | 7616999008 | OTHER ALUMINUM PRODUCTS: BUSHING (P/N D59885). DIMENSIONS: 200X100X100 MM. THICKNESS: 4 MM. BODY MATERIAL: ALUMINUM ALLOY. MANUFACTURING METHOD: STAMPING. IT IS INSTALLED ON THE WHEEL FASTENING AXIS OF THE AIRCRAFT CHASSIS FRONT SUPPORT. SERVES TO PROTECT THE AXIS FROM | 0.28 | 909.76 | France | MUNICH AIRPORT | AIRLINE RUSSIA JSC |
1/28/2022 | 7616999008 | TECHNOLOGICAL HATCH OF THE PANEL OF THE FRONT PILLAR OF THE CHASSIS OF A BOEING 737 CIVIL AVIATION: | 1.32 | 5190 | Israel | SEATTLE AIRPORT USA | S 7 ENGINEERING LLC |
1/22/2022 | 7616999008 | BRACKET OF THE POWER SET OF THE FRONT PILLAR NICHE OF THE CHASSIS OF A319/320 CIVIL AVIATION: | 0.03 | 668.42 | France | HAMBURG AIRPORT GERMANY | S 7 ENGINEERING LLC |
1/21/2022 | 7616999008 | FASTENING MANIFOLD OF THE FRONT CHASSIS TURN CONTROL SYSTEM, ON THE CEILING PANEL OF THE CHASSIS COMPARTMENT OF THE PASSENGER GA EMBRAER 170/175 ASSEMBLY. MATERIAL - ALUMINUM ALLOY (90% ALUMINUM, 10% ADDITIVES). P/N: | 0.09 | 170.83 | France | MITRI MORI | S 7 ENGINEERING LLC |
1/24/2022 | 7616999008 | FASTENING ASSEMBLY FOR THE SEAL OF THE RIGHT FASHION OF THE FRONT PILLAR OF THE CHASSIS BOEING 737 OF CIVIL AVIATION, MATERIAL: ALUMINUM (ALUMINUM 97%, IMPURITY 3%), STAMPING, GALVANIC TREATMENT. | 0.2 | 1312.23 | United States of America | SEATAC | S 7 ENGINEERING LLC |
1/16/2022 | 7616999008 | THE ALUMINUM ALLOY WHEEL CAP HAS A FLANGE WITH INSTALLATION HOLES. SERVES TO PROTECT THE WHEEL HUB OF THE FRONT POST CHASSIS OF THE EMBRAER 145 PASSENGER ACFT GA AGAINST MOISTURE AND DIRT. USED FOR REPAIR AND MAINTENANCE | 0.09 | 701.03 | United States of America | DALLAS FORT WORTH AIRPORT | S 7 ENGINEERING LLC |