1/4/2022 | 8108909008 | PLATE H/N 143A8333-8, MADE OF TITANIUM ALLOYS (CHEMICAL COMPOSITION: 87% TITANIUM, 10% ALUMINUM, 3% NICKEL) TECHNICAL | 2.29 | 1602.32 | United States of America | SUNRISE | PJSC AIRLINE UTair |
1/8/2022 | 8108909008 | SCREW PN BACB30VF4K5 WITH A CROSS HEAD SCREW MADE FROM TITANIUM ALLOY (TITANIUM - 90%, ALUMINUM - 6%, VANADIUM - 4%). NOMINAL THREAD DIAMETER 6 MM. FOR INSTALLATION IN THE MOUNTS OF FASTENING OF THE STRUCTURAL ELEMENTS OF THE AC AC. FOR TECHNICAL | 0.45 | 727 | United States of America | KANSAS CITY AIRPORT | RED WINGS JSC |
1/29/2022 | 8108909008 | REAR BOOT SILL B/N 146A8342-8, MADE FROM TITANIUM ALLOYS (CHEMICAL COMPOSITION: TITANIUM-88%, ALUMINUM-6.5%, VANADIUM-4.5%, IRON-0.25), BY STAMPING METHOD, WITH SUBSEQUENT TURNING, AND FINISHING WITH TECHNOLOGICAL HOLES FOR K | 1.58 | 3121.6 | United States of America | TEMPE | PJSC AIRLINE UTair |
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 |