4075339: SEAL,AIR,AIRCRAFT GAS TURBINE EN.
SEAL,AIR,AIRCRAFT GAS TURBINE EN. Key specifications include material: STEEL OVERALL, design_type: AXIAL COMPRESSOR, overall_length: 2.636 INCHES NOMINAL IN, hardness_rating: 25.0 ROCKWELL C MINIMUM AND 33.0 ROCKWELL C MAXIMUM OVERALL, special_features: T.O. 2J-F100-54, material_thickness: 0.060 INCHES NOMINAL IN.
This part is cataloged in the U.S. Government catalog under NSN 2840-01-321-4457, 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 | STEEL OVERALL |
| design_type | AXIAL COMPRESSOR |
| stage_number | 1 |
| overall_length | 2.636 INCHES NOMINAL IN |
| hardness_rating | 25.0 ROCKWELL C MINIMUM AND 33.0 ROCKWELL C MAXIMUM OVERALL |
| special_features | T.O. 2J-F100-54 |
| material_thickness | 0.060 INCHES NOMINAL IN |
| end_item_identification | F100PW0229 AIRCRAFT ENGINE |
| engine_section_location | LOW PRESSURE COMPRESSOR |
| criticality_code_justification | AGAV |
| material_document_and_classification | AMS5613 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| NSN | 2840-01-321-4457 |
| STAGE NUMBER | 1 |
| DESIGN TYPE | AXIAL COMPRESSOR |
| HARDNESS RATING | 25.0 ROCKWELL C MINIMUM AND 33.0 ROCKWELL C MAXIMUM OVERALL |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| MATERIAL DOCUMENT AND CLASSIFICATION | AMS5613 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| OVERALL LENGTH | 2.636 INCHES NOMINAL IN |
| ENGINE SECTION LOCATION | LOW PRESSURE COMPRESSOR |
| MATERIAL THICKNESS | 0.060 INCHES NOMINAL IN |
| SPECIAL FEATURES | T.O. 2J-F100-54 |
| END ITEM IDENTIFICATION | F100PW0229 AIRCRAFT ENGINE |
No substitute or cross-reference records for this part.