2189814: NOZZLE,TURBINE,AIRCRAFT GAS TURB.
NOZZLE,TURBINE,AIRCRAFT GAS TURB. Key specifications include material: NICKEL ALLOY OVERALL, overall_width: 3.080 INCHES NOMINAL IN, overall_length: 9.732 INCHES MINIMUM AND 9.832 INCHES MAXIMUM IN, material_thickness: 0.018 INCHES MINIMUM AND 0.021 INCHES MAXIMUM IN, engine_section_location: TURBINE, material_document_and_classification: AMS5544 ASSN STD SINGLE MATERIAL RESPONSE OVERALL. This part is cataloged in the U.S.
Government catalog under NSN 2840-01-339-7016, 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_width | 3.080 INCHES NOMINAL IN |
| overall_length | 9.732 INCHES MINIMUM AND 9.832 INCHES MAXIMUM IN |
| material_thickness | 0.018 INCHES MINIMUM AND 0.021 INCHES MAXIMUM IN |
| engine_section_location | TURBINE |
| material_document_and_classification | AMS5544 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| part_name_assigned_by_controlling_agency | NOZZLE,TURBINE,TURBINE ENGINE |
| NSN | 2840-01-339-7016 |
| MATERIAL DOCUMENT AND CLASSIFICATION | AMS5544 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| OVERALL LENGTH | 9.732 INCHES MINIMUM AND 9.832 INCHES MAXIMUM IN |
| OVERALL WIDTH | 3.080 INCHES NOMINAL IN |
| ENGINE SECTION LOCATION | TURBINE |
| MATERIAL THICKNESS | 0.018 INCHES MINIMUM AND 0.021 INCHES MAXIMUM IN |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | NOZZLE,TURBINE,TURBINE ENGINE |
| MATERIAL | NICKEL ALLOY OVERALL |
No substitute or cross-reference records for this part.