673723: PLATE,COMPONENT MOUNTING,AIRCRAF.
PLATE,COMPONENT MOUNTING,AIRCRAF. Key specifications include material: NICKEL ALLOY OVERALL, overall_width: 0.203 INCHES MINIMUM AND 0.233 INCHES MAXIMUM IN, overall_length: 0.880 INCHES MINIMUM AND 0.920 INCHES MAXIMUM IN, end_item_identification: TF-30 AIRCRAFT GAS TURBINE ENGINE, engine_section_location: COMBUSTION CHAMBER, criticality_code_justification: CZBJ AND ABHP AND ABMK AND AGAV. This part is cataloged in the U.S.
Government catalog under NSN 2840-00-184-4980, 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 | 0.203 INCHES MINIMUM AND 0.233 INCHES MAXIMUM IN |
| overall_length | 0.880 INCHES MINIMUM AND 0.920 INCHES MAXIMUM IN |
| end_item_identification | TF-30 AIRCRAFT GAS TURBINE ENGINE |
| engine_section_location | COMBUSTION CHAMBER |
| criticality_code_justification | CZBJ AND ABHP AND ABMK AND AGAV |
| material_document_and_classification | AMS5536 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| part_name_assigned_by_controlling_agency | ORIGINAL NAME BOSS,CHAMBER,COMBUSTION |
| NSN | 2840-00-184-4980 |
| CRITICALITY CODE JUSTIFICATION | CZBJ AND ABHP AND ABMK AND AGAV |
| MATERIAL DOCUMENT AND CLASSIFICATION | AMS5536 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| OVERALL LENGTH | 0.880 INCHES MINIMUM AND 0.920 INCHES MAXIMUM IN |
| OVERALL WIDTH | 0.203 INCHES MINIMUM AND 0.233 INCHES MAXIMUM IN |
| ENGINE SECTION LOCATION | COMBUSTION CHAMBER |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | ORIGINAL NAME BOSS,CHAMBER,COMBUSTION |
| END ITEM IDENTIFICATION | TF-30 AIRCRAFT GAS TURBINE ENGINE |
| MATERIAL | NICKEL ALLOY OVERALL |
No substitute or cross-reference records for this part.