9502M36P01: SEAL,AIR,AIRCRAFT GAS TURBINE EN.
SEAL,AIR,AIRCRAFT GAS TURBINE EN. Key specifications include diameter: 5.588 INCHES MINIMUM AND 5.592 INCHES MAXIMUM IN, material: STEEL OVERALL, overall_width: 0.138 INCHES MINIMUM AND 0.142 INCHES MAXIMUM IN, overall_length: 0.860 INCHES MINIMUM AND 0.880 INCHES MAXIMUM IN, hardness_rating: 28.0 ROCKWELL C MINIMUM AND 37.0 ROCKWELL C MAXIMUM OVERALL, special_features: T.O. 2J-F110-14.
This part is cataloged in the U.S. Government catalog under NSN 2840-01-146-5654, 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 | 5.588 INCHES MINIMUM AND 5.592 INCHES MAXIMUM IN |
| material | STEEL OVERALL |
| overall_width | 0.138 INCHES MINIMUM AND 0.142 INCHES MAXIMUM IN |
| overall_length | 0.860 INCHES MINIMUM AND 0.880 INCHES MAXIMUM IN |
| hardness_rating | 28.0 ROCKWELL C MINIMUM AND 37.0 ROCKWELL C MAXIMUM OVERALL |
| special_features | T.O. 2J-F110-14 |
| end_item_identification | F101/F110GE129 AIRCRAFT ENGINE |
| engine_section_location | TURBINE |
| criticality_code_justification | AGAV |
| material_document_and_classification | AMS5643 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| NSN | 2840-01-146-5654 |
| HARDNESS RATING | 28.0 ROCKWELL C MINIMUM AND 37.0 ROCKWELL C MAXIMUM OVERALL |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| MATERIAL DOCUMENT AND CLASSIFICATION | AMS5643 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| DIAMETER | 5.588 INCHES MINIMUM AND 5.592 INCHES MAXIMUM IN |
| OVERALL LENGTH | 0.860 INCHES MINIMUM AND 0.880 INCHES MAXIMUM IN |
| OVERALL WIDTH | 0.138 INCHES MINIMUM AND 0.142 INCHES MAXIMUM IN |
| ENGINE SECTION LOCATION | TURBINE |
| SPECIAL FEATURES | T.O. 2J-F110-14 |
| END ITEM IDENTIFICATION | F101/F110GE129 AIRCRAFT ENGINE |
| MATERIAL | STEEL OVERALL |
No substitute or cross-reference records for this part.