705359: SHIELD,HEAT,AIRCRAFT GAS TURBINE.
SHIELD,HEAT,AIRCRAFT GAS TURBINE. Key specifications include diameter: 11.730 INCHES MINIMUM AND 11.770 INCHES MAXIMUM IN, material: STEEL COMP 410 SHIELD, overall_length: 4.260 INCHES MINIMUM AND 4.300 INCHES MAXIMUM IN, hardness_rating: 25.0 ROCKWELL C MINIMUM AND 33.0 ROCKWELL C MAXIMUM SHIELD, end_item_identification: TF-33 AIRCRAFT ENGINE, engine_section_location: TURBINE. This part is cataloged in the U.S.
Government catalog under NSN 2840-00-138-6760, 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 | 11.730 INCHES MINIMUM AND 11.770 INCHES MAXIMUM IN |
| material | STEEL COMP 410 SHIELD |
| overall_length | 4.260 INCHES MINIMUM AND 4.300 INCHES MAXIMUM IN |
| hardness_rating | 25.0 ROCKWELL C MINIMUM AND 33.0 ROCKWELL C MAXIMUM SHIELD |
| end_item_identification | TF-33 AIRCRAFT ENGINE |
| engine_section_location | TURBINE |
| material_document_and_classification | AMS5504 ASSN STD SINGLE MATERIAL RESPONSE SHIELD |
| NSN | 2840-00-138-6760 |
| HARDNESS RATING | 25.0 ROCKWELL C MINIMUM AND 33.0 ROCKWELL C MAXIMUM SHIELD |
| MATERIAL DOCUMENT AND CLASSIFICATION | AMS5504 ASSN STD SINGLE MATERIAL RESPONSE SHIELD |
| DIAMETER | 11.730 INCHES MINIMUM AND 11.770 INCHES MAXIMUM IN |
| OVERALL LENGTH | 4.260 INCHES MINIMUM AND 4.300 INCHES MAXIMUM IN |
| ENGINE SECTION LOCATION | TURBINE |
| END ITEM IDENTIFICATION | TF-33 AIRCRAFT ENGINE |
| MATERIAL | STEEL COMP 410 SHIELD |
No substitute or cross-reference records for this part.