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 |
1/6/2022 | 7318220008 | FLAT, WASHER, INNER DIAMETER 25 MM. USED IN THE ASSEMBLY OF THE ENGINE ENGINE OF A BOEING 737 CITIZEN. AVIATION: | 0.09 | 43.61 | United States of America | SEATLE | S 7 ENGINEERING LLC |
1/6/2022 | 7318220008 | ROUND WASHER, FLAT, NOT SPLIT, NOT LOCKING, USED WHEN INSTALLING THE HOOD LOCK OF THE MAIN ENGINE OF PASSENGER AIRBUS 319/320 CIVIL AVIATION. DIAMETER 5 MM. MATERIAL - CORROSION-RESISTANT STEEL : | 0.08 | 195.22 | United States of America | TOULOUSE AIRPORT | S 7 ENGINEERING LLC |
1/6/2022 | 7318220008 | THE WASHER IS FLAT, ROUND, NOT LOCKING, NOT SPRING, NOT SPLIT, IS USED WHEN INSTALLING THE NOZZLE UNIT ON THE MAIN ENGINE BODY OF AIRBUS A319/A320/A321 CIVIL AVIATION PASSENGER AIRCRAFT. DIAMETER 10 MM : | 0.01 | 16.36 | United States of America | TOULOUSE AIRPORT | S 7 ENGINEERING LLC |
1/15/2022 | 7318220008 | NON-LOCK WASHER, NON SPRING, SINGLE-WIND, MADE OF CORROSION-RESISTANT STEEL, ROUND SHAPE, FLAT, USED IN THE STRUCTURE OF THE REAR ASSEMBLY OF THE LINKAGE OF THE MAIN ENGINE OF AIRBUS A319/A320/A321 PASSENGER AIRCRAFT | 0.14 | 764.94 | United States of America | TOULOUSE AIRPORT | S 7 ENGINEERING LLC |
1/15/2022 | 7318220008 | NON-LOCK WASHER, NON SPRING, SINGLE WIND, MADE OF CORROSION-RESISTANT STEEL, ROUND SHAPE, FLAT, USED IN THE STRUCTURE OF THE FRONT HINGE UNIT OF THE MAIN ENGINE OF AIRBUS A319/A320/A321 PASSENGER AC | 0.1 | 302.85 | United States of America | TOULOUSE AIRPORT | S 7 ENGINEERING LLC |