KH14134 J#&COMPONENTS TO BE INSTALLED IN THE ENGINE IN THE MIDDLE HEATING STAGE TO ENSURE THE TEMPERATURE AND PRESSURE RATIO IN THE AIRCRAFT ENGINE TURBINE SIZE 113*33*51MM#&VN
KH14134 J#&COMPONENTS TO BE INSTALLED IN THE ENGINE IN THE MIDDLE HEATING STAGE TO ENSURE THE TEMPERATURE AND PRESSURE RATIO IN THE AIRCRAFT ENGINE TURBINE SIZE 113*33*51MM#&VN
28-October-2022
8411910000
KH10570 E#&COMPONENTS FOR MOUNTING IN THE ENGINE IN THE HIGH HEATING STAGE TO ENSURE THE TEMPERATURE AND PRESSURE RATIO IN THE AIRCRAFT ENGINE TURBINE SIZE 112*55*40#&EN
KH10570 E#&COMPONENTS FOR MOUNTING IN THE ENGINE IN THE HIGH HEATING STAGE TO ENSURE THE TEMPERATURE AND PRESSURE RATIO IN THE AIRCRAFT ENGINE TURBINE SIZE 112*55*40#&EN
23-March-2023
8411910000
KH10568 C#&COMPONENTS TO BE INSTALLED IN THE ENGINE IN THE HIGH HEATING STAGE TO ENSURE THE TEMPERATURE AND PRESSURE RATIO IN THE AIRCRAFT ENGINE TURBINE SIZE 112*36*29#&VN
KH10568 C#&COMPONENTS TO BE INSTALLED IN THE ENGINE IN THE HIGH HEATING STAGE TO ENSURE THE TEMPERATURE AND PRESSURE RATIO IN THE AIRCRAFT ENGINE TURBINE SIZE 112*36*29#&VN
28-March-2023
8411910000
30G6292 A#&NICKEL ALLOY HIGH-PRESSURE TURBINE HOUSING DIMENSIONS 561.1 X 453.6 X 192.3 (OD X ID X H) AIRCRAFT ENGINE ASSEMBLY COMPONENTS#&EN
30G6292 A#&NICKEL ALLOY HIGH-PRESSURE TURBINE HOUSING DIMENSIONS 561.1 X 453.6 X 192.3 (OD X ID X H) AIRCRAFT ENGINE ASSEMBLY COMPONENTS#&EN