4067004: BLADE,TURBINE ROTOR,AIRCRAFT GAS.
BLADE,TURBINE ROTOR,AIRCRAFT GAS. Key specifications include material: NICKEL ALLOY BLADE, overall_length: 6.660 INCHES MINIMUM AND 6.670 INCHES MAXIMUM IN, end_item_identification: ACFT ENG. F100/200/200A A, engine_section_location: TURBINE, material_document_and_classification: PWA658 ASSN STD SINGLE MATERIAL RESPONSE BLADE.
This part is cataloged in the U.S. Government catalog under NSN 2840-01-224-9266, 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 | NICKEL ALLOY BLADE |
| stage_number | 4 |
| overall_length | 6.660 INCHES MINIMUM AND 6.670 INCHES MAXIMUM IN |
| end_item_identification | ACFT ENG. F100/200/200A A |
| engine_section_location | TURBINE |
| material_document_and_classification | PWA658 ASSN STD SINGLE MATERIAL RESPONSE BLADE |
| NSN | 2840-01-224-9266 |
| STAGE NUMBER | 4 |
| MATERIAL DOCUMENT AND CLASSIFICATION | PWA658 ASSN STD SINGLE MATERIAL RESPONSE BLADE |
| OVERALL LENGTH | 6.660 INCHES MINIMUM AND 6.670 INCHES MAXIMUM IN |
| ENGINE SECTION LOCATION | TURBINE |
| END ITEM IDENTIFICATION | ACFT ENG. F100/200/200A A |
| MATERIAL | NICKEL ALLOY BLADE |
No substitute or cross-reference records for this part.