4078430: CASE,FAN,AIRCRAFT GAS TURBINE EN.
CASE,FAN,AIRCRAFT GAS TURBINE EN. Key specifications include diameter: 36.260 INCHES MINIMUM AND 36.280 INCHES MAXIMUM IN, material: TITANIUM ALLOY OVERALL, design_type: AXIAL COMPRESSOR, overall_length: 1.882 INCHES MINIMUM AND 1.912 INCHES MAXIMUM IN, special_features: 1ST STAGE, end_item_identification: F100-PW-100/200/220 AIRCRAFT GAS TURBINE ENGINE. This part is cataloged in the U.S.
Government catalog under NSN 2840-01-395-7432, 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 | 36.260 INCHES MINIMUM AND 36.280 INCHES MAXIMUM IN |
| material | TITANIUM ALLOY OVERALL |
| design_type | AXIAL COMPRESSOR |
| overall_length | 1.882 INCHES MINIMUM AND 1.912 INCHES MAXIMUM IN |
| special_features | 1ST STAGE |
| end_item_identification | F100-PW-100/200/220 AIRCRAFT GAS TURBINE ENGINE |
| engine_section_location | FAN |
| criticality_code_justification | APGF AND CZBJ AND ABMZ AND FEAT |
| material_document_and_classification | AMS4928 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| NSN | 2840-01-395-7432 |
| DESIGN TYPE | AXIAL COMPRESSOR |
| CRITICALITY CODE JUSTIFICATION | APGF AND CZBJ AND ABMZ AND FEAT |
| MATERIAL DOCUMENT AND CLASSIFICATION | AMS4928 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| DIAMETER | 36.260 INCHES MINIMUM AND 36.280 INCHES MAXIMUM IN |
| OVERALL LENGTH | 1.882 INCHES MINIMUM AND 1.912 INCHES MAXIMUM IN |
| ENGINE SECTION LOCATION | FAN |
| SPECIAL FEATURES | 1ST STAGE |
| END ITEM IDENTIFICATION | F100-PW-100/200/220 AIRCRAFT GAS TURBINE ENGINE |
| MATERIAL | TITANIUM ALLOY OVERALL |
No substitute or cross-reference records for this part.