4059462: CASE,TURBINE,AIRCRAFT GAS TURBIN.
CASE,TURBINE,AIRCRAFT GAS TURBIN. Key specifications include diameter: 19.267 INCHES MINIMUM AND 19.269 INCHES MAXIMUM IN, material: NICKEL ALLOY OVERALL, overall_length: 3.570 INCHES MINIMUM AND 3.580 INCHES MAXIMUM IN, special_features: ORIGINAL NAME: CASE,TURBINE ROTOR,TURBINE ENGINE; STAGE 12, end_item_identification: ACFT ENG F100, engine_section_location: TURBINE. This part is cataloged in the U.S.
Government catalog under NSN 2840-01-138-5776, 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 | 19.267 INCHES MINIMUM AND 19.269 INCHES MAXIMUM IN |
| material | NICKEL ALLOY OVERALL |
| overall_length | 3.570 INCHES MINIMUM AND 3.580 INCHES MAXIMUM IN |
| special_features | ORIGINAL NAME: CASE,TURBINE ROTOR,TURBINE ENGINE; STAGE 12 |
| end_item_identification | ACFT ENG F100 |
| engine_section_location | TURBINE |
| criticality_code_justification | ABHP AND ABMZ AND CZBJ AND FEAT |
| material_document_and_classification | AMS5707 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| NSN | 2840-01-138-5776 |
| CRITICALITY CODE JUSTIFICATION | ABHP AND ABMZ AND CZBJ AND FEAT |
| MATERIAL DOCUMENT AND CLASSIFICATION | AMS5707 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| DIAMETER | 19.267 INCHES MINIMUM AND 19.269 INCHES MAXIMUM IN |
| OVERALL LENGTH | 3.570 INCHES MINIMUM AND 3.580 INCHES MAXIMUM IN |
| ENGINE SECTION LOCATION | TURBINE |
| SPECIAL FEATURES | ORIGINAL NAME: CASE,TURBINE ROTOR,TURBINE ENGINE; STAGE 12 |
| END ITEM IDENTIFICATION | ACFT ENG F100 |
| MATERIAL | NICKEL ALLOY OVERALL |
No substitute or cross-reference records for this part.