30G4185-01 B # & HIGH PRESSURE TURBINE SHELLS OF AIRCRAFT ENGINES NICKEL ALLOY DETAILS ASSEMBLY IN AIRCRAFT ENGINE (NW: 70 KG / 02 PCS) # & VN
30G4185-01 B # & HIGH PRESSURE TURBINE SHELLS OF AIRCRAFT ENGINES NICKEL ALLOY DETAILS ASSEMBLY IN AIRCRAFT ENGINE (NW: 70 KG / 02 PCS) # & VN
17-September-2021
8411990000
30G4185-01 B # & HIGH PRESSURE TURBINE SHELLS OF AIRCRAFT ENGINE NICKEL ALLOY DETAILS ASSEMBLY IN AIRCRAFT ENGINE (NW: 35 KGS / 01 PCS) # & VN
30G4185-01 B # & HIGH PRESSURE TURBINE SHELLS OF AIRCRAFT ENGINE NICKEL ALLOY DETAILS ASSEMBLY IN AIRCRAFT ENGINE (NW: 35 KGS / 01 PCS) # & VN
20-April-2022
8411990000
KH57053 F#& TURBINE DETAILS HIGH PRESSURE AREA WITH NICKEL ALLOY KT 100 X 55 X 35 (MM) USE TO ENSURE THE RATIO OF HIGH TEMPERATURES AND PRESSURE IN AIRCRAFT ENGINE TURBINE (NW: 45 KGS/75 PCS) #&VN
KH57053 F#& TURBINE DETAILS HIGH PRESSURE AREA WITH NICKEL ALLOY KT 100 X 55 X 35 (MM) USE TO ENSURE THE RATIO OF HIGH TEMPERATURES AND PRESSURE IN AIRCRAFT ENGINE TURBINE (NW: 45 KGS/75 PCS) #&VN
20-April-2022
8411990000
KH57053 F#& TURBINE DETAILS OF HIGH PRESSURE AREA WITH NICKEL ALLOY KT 100 X 55 X 35 (MM) USE TO ENSURE THE RATIO OF HIGH TEMPERATURES AND PRESSURE IN AIRCRAFT ENGINE TURBINE (NW: 19.2KGS/ 32PCS)# &VN
KH57053 F#& TURBINE DETAILS OF HIGH PRESSURE AREA WITH NICKEL ALLOY KT 100 X 55 X 35 (MM) USE TO ENSURE THE RATIO OF HIGH TEMPERATURES AND PRESSURE IN AIRCRAFT ENGINE TURBINE (NW: 19.2KGS/ 32PCS)# &VN