33A.1396 A#&AIRCRAFT ENGINE INNER WING DETAIL IN NICKEL ALLOY#&EN
33A.1396 A#&AIRCRAFT ENGINE INNER WING DETAIL IN NICKEL ALLOY#&EN
04-November-2022
8411910000
KH1.0568 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
KH1.0568 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
09-December-2022
8411910000
KH1.4134 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
KH1.4134 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
02-December-2022
8411910000
KH1.0570 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
KH1.0570 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