CABLE ASSEMBLY,SPECIAL PURPOSE,E. Key specifications include material: NICKEL ALLOY OVERALL, overall_length: 1.590 INCHES MINIMUM AND 1.610 INCHES MAXIMUM IN, end_item_identification: TF-30 AIRCRAFT GAS TURBINE ENGINE, engine_section_location: COMBUSTION CHAMBER, criticality_code_justification: CZBJ AND ABHP AND AGAV, material_document_and_classification: AMS5536 ASSN STD SINGLE MATERIAL RESPONSE OVERALL. This product is currently in active production with full OEM support.
This part is cataloged in the Federal Logistics Information System (FLIS) under NSN 2840-00-003-9754, 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 OVERALL |
| overall_length | 1.590 INCHES MINIMUM AND 1.610 INCHES MAXIMUM IN |
| end_item_identification | TF-30 AIRCRAFT GAS TURBINE ENGINE |
| engine_section_location | COMBUSTION CHAMBER |
| criticality_code_justification | CZBJ AND ABHP AND AGAV |
| material_document_and_classification | AMS5536 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| part_name_assigned_by_controlling_agency | ORIGINAL NAME BOSS,COMBUSTION CHAMBER,TURBINE ENGINE |
| NSN | 2840-00-003-9754 |
| END ITEM IDENTIFICATION | TF-30 AIRCRAFT GAS TURBINE ENGINE |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | ORIGINAL NAME BOSS,COMBUSTION CHAMBER,TURBINE ENGINE |
| ENGINE SECTION LOCATION | COMBUSTION CHAMBER |
| MATERIAL DOCUMENT AND CLASSIFICATION | AMS5536 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| OVERALL LENGTH | 1.590 INCHES MINIMUM AND 1.610 INCHES MAXIMUM IN |
| CRITICALITY CODE JUSTIFICATION | CZBJ AND ABHP AND AGAV |
| MATERIAL | NICKEL ALLOY OVERALL |