SEAL,AIR,AIRCRAFT GAS TURBINE EN. Key specifications include diameter: 20.342 INCHES MINIMUM AND 20.346 INCHES MAXIMUM IN, material: STEEL OVERALL, design_type: COMPRESSOR, overall_length: 0.810 INCHES MINIMUM AND 0.820 INCHES MAXIMUM IN, hardness_rating: 35.0 ROCKWELL C NOMINAL AND 40.0 ROCKWELL C MINIMUM OVERALL, special_features: MATERIAL MODIFIED PER SPEC SUPPLEMENT PWA-S-6304. This product is currently in active production with full OEM support.
This part is cataloged in the Federal Logistics Information System (FLIS) under NSN 2920-00-500-2133, 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.
| diameter | 20.342 INCHES MINIMUM AND 20.346 INCHES MAXIMUM IN |
| material | STEEL OVERALL |
| design_type | COMPRESSOR |
| overall_length | 0.810 INCHES MINIMUM AND 0.820 INCHES MAXIMUM IN |
| hardness_rating | 35.0 ROCKWELL C NOMINAL AND 40.0 ROCKWELL C MINIMUM OVERALL |
| special_features | MATERIAL MODIFIED PER SPEC SUPPLEMENT PWA-S-6304 |
| end_item_identification | TF-33 AIRCRAFT ENGINE |
| engine_section_location | COMPRESSOR |
| criticality_code_justification | APGF AND CZBJ AND ABHP AND ABMZ AND CQFM |
| material_document_and_classification | AMS6304 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| NSN | 2920-00-500-2133 |
| OVERALL LENGTH | 10.7500 INCHES NOMINAL IN |
| OVERALL DIAMETER | 2.5000 INCHES NOMINAL IN |
| FEATURES PROVIDED | SHAFT |
| CONSTRUCTION | SLOT WOUND |