P311P04: BLADE,COMPRESSOR,AIRCRAFT GAS TU.
BLADE,COMPRESSOR,AIRCRAFT GAS TU. Key specifications include material: TITANIUM ALLOY BLADE, design_type: AXIAL COMPRESSOR, overall_length: 3.798 INCHES NOMINAL IN, special_features: BLADE IS DOVETAIL, end_item_identification: F110GE129 AIRCRAFT ENGINE, engine_section_location: COMPRESSOR. This part is cataloged in the U.S.
Government catalog under NSN 2840-01-322-4757, 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 | TITANIUM ALLOY BLADE |
| design_type | AXIAL COMPRESSOR |
| stage_number | 1 |
| overall_length | 3.798 INCHES NOMINAL IN |
| special_features | BLADE IS DOVETAIL |
| end_item_identification | F110GE129 AIRCRAFT ENGINE |
| engine_section_location | COMPRESSOR |
| criticality_code_justification | AGAV |
| NSN | 2840-01-322-4757 |
| STAGE NUMBER | 1 |
| DESIGN TYPE | AXIAL COMPRESSOR |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| OVERALL LENGTH | 3.798 INCHES NOMINAL IN |
| ENGINE SECTION LOCATION | COMPRESSOR |
| SPECIAL FEATURES | BLADE IS DOVETAIL |
| END ITEM IDENTIFICATION | F110GE129 AIRCRAFT ENGINE |
| MATERIAL | TITANIUM ALLOY BLADE |
No substitute or cross-reference records for this part.