1360M80G23: FRAME,TURBINE,AIRCRAFT GAS TURBI.
FRAME,TURBINE,AIRCRAFT GAS TURBI. Key specifications include material: NICKEL ALLOY, end_item_identification: F118-GE-100, reference_data_and_literature: 2J-F118-4 FIG59 IND1, criticality_code_justification: AGAV, number_of_variable_guide_vanes: 10, material_document_and_classification: AMS5536 ASSN STD SINGLE MATERIAL RESPONSE. This part is cataloged in the U.S.
Government catalog under NSN 2840-01-507-8523, indicating validated use in U.S. government and defense logistics supply chains. Available through authorized enterprise resellers and TPM (Third Party Maintenance) channels.
Verify compatibility with your specific system configuration before ordering.
| material | NICKEL ALLOY |
| end_item_identification | F118-GE-100 |
| reference_data_and_literature | 2J-F118-4 FIG59 IND1 |
| criticality_code_justification | AGAV |
| number_of_variable_guide_vanes | 10 |
| material_document_and_classification | AMS5536 ASSN STD SINGLE MATERIAL RESPONSE |
| NSN | 2840-01-507-8523 |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| REFERENCE DATA AND LITERATURE | 2J-F118-4 FIG59 IND1 |
| MATERIAL DOCUMENT AND CLASSIFICATION | AMS5536 ASSN STD SINGLE MATERIAL RESPONSE |
| NUMBER OF VARIABLE GUIDE VANES | 10 |
| END ITEM IDENTIFICATION | F118-GE-100 |
| MATERIAL | NICKEL ALLOY |
No substitute or cross-reference records for this part.