P104P02: BLADE,COMPRESSOR,AIRCRAFT GAS TU.
BLADE,COMPRESSOR,AIRCRAFT GAS TU. Key specifications include material: NICKEL ALLOY BLADE, design_type: COMPRESSOR, overall_width: 0.935 INCHES MINIMUM AND 0.939 INCHES MAXIMUM IN, overall_length: 1.934 INCHES NOMINAL IN, special_features: ORIGINAL NAME BLADE,COMPRESSOR ROTOR,TURBINE ENGINE, end_item_identification: ACFT ENG F101-GE-100,F108-CF-100,AND F110-GE-100. This part is cataloged in the U.S.
Government catalog under NSN 2840-01-147-1859, 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 |
| design_type | COMPRESSOR |
| stage_number | 4 |
| overall_width | 0.935 INCHES MINIMUM AND 0.939 INCHES MAXIMUM IN |
| overall_length | 1.934 INCHES NOMINAL IN |
| special_features | ORIGINAL NAME BLADE,COMPRESSOR ROTOR,TURBINE ENGINE |
| end_item_identification | ACFT ENG F101-GE-100,F108-CF-100,AND F110-GE-100 |
| engine_section_location | LOW PRESSURE COMPRESSOR |
| criticality_code_justification | AGAV |
| NSN | 2840-01-147-1859 |
| STAGE NUMBER | 4 |
| DESIGN TYPE | COMPRESSOR |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| OVERALL LENGTH | 1.934 INCHES NOMINAL IN |
| OVERALL WIDTH | 0.935 INCHES MINIMUM AND 0.939 INCHES MAXIMUM IN |
| ENGINE SECTION LOCATION | LOW PRESSURE COMPRESSOR |
| SPECIAL FEATURES | ORIGINAL NAME BLADE,COMPRESSOR ROTOR,TURBINE ENGINE |
| END ITEM IDENTIFICATION | ACFT ENG F101-GE-100,F108-CF-100,AND F110-GE-100 |
| MATERIAL | NICKEL ALLOY BLADE |
No substitute or cross-reference records for this part.