4062757: CASE,TURBINE,AIRCRAFT GAS TURBIN.
CASE,TURBINE,AIRCRAFT GAS TURBIN. Key specifications include diameter: 16.890 INCHES MINIMUM AND 16.892 INCHES MAXIMUM IN, material: NICKEL ALLOY OVERALL, overall_length: 1.415 INCHES MINIMUM AND 1.425 INCHES MAXIMUM IN, special_features: WAS CASE,TURBINE ROTOR,TURBINE ENGINE, end_item_identification: ACFT ENG F100-PW-100/200/200A A, engine_section_location: TURBINE. This part is cataloged in the U.S.
Government catalog under NSN 2840-01-215-7606, 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 | 16.890 INCHES MINIMUM AND 16.892 INCHES MAXIMUM IN |
| material | NICKEL ALLOY OVERALL |
| overall_length | 1.415 INCHES MINIMUM AND 1.425 INCHES MAXIMUM IN |
| special_features | WAS CASE,TURBINE ROTOR,TURBINE ENGINE |
| end_item_identification | ACFT ENG F100-PW-100/200/200A A |
| engine_section_location | TURBINE |
| criticality_code_justification | AGAV |
| material_document_and_classification | AMS5662 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| NSN | 2840-01-215-7606 |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| MATERIAL DOCUMENT AND CLASSIFICATION | AMS5662 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| DIAMETER | 16.890 INCHES MINIMUM AND 16.892 INCHES MAXIMUM IN |
| OVERALL LENGTH | 1.415 INCHES MINIMUM AND 1.425 INCHES MAXIMUM IN |
| ENGINE SECTION LOCATION | TURBINE |
| SPECIAL FEATURES | WAS CASE,TURBINE ROTOR,TURBINE ENGINE |
| END ITEM IDENTIFICATION | ACFT ENG F100-PW-100/200/200A A |
| MATERIAL | NICKEL ALLOY OVERALL |
No substitute or cross-reference records for this part.