4068008: DISK,COMPRESSOR,AIRCRAFT GAS TUR.
DISK,COMPRESSOR,AIRCRAFT GAS TUR. Key specifications include material: NICKEL ALLOY OVERALL, design_type: AXIAL COMPRESSOR, overall_length: 0.813 INCHES NOMINAL IN, special_features: T.O. 2J-F100-4 FIG 130 IND 4; 2J-F100-14 FIG 136 IND 3, fsc_application_data: F-15 AIRCRAFT, end_item_identification: ACFT ENG F100-PW-100/200.
This part is cataloged in the U.S. Government catalog under NSN 2840-01-214-9902, 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 OVERALL |
| design_type | AXIAL COMPRESSOR |
| stage_number | 8 |
| overall_length | 0.813 INCHES NOMINAL IN |
| special_features | T.O. 2J-F100-4 FIG 130 IND 4; 2J-F100-14 FIG 136 IND 3 |
| fsc_application_data | F-15 AIRCRAFT |
| end_item_identification | ACFT ENG F100-PW-100/200 |
| engine_section_location | COMPRESSOR |
| part_name_assigned_by_controlling_agency | ORIG NAME DISK,GAS TURBINE ENG |
| NSN | 2840-01-214-9902 |
| FSC APPLICATION DATA | F-15 AIRCRAFT |
| STAGE NUMBER | 8 |
| DESIGN TYPE | AXIAL COMPRESSOR |
| OVERALL LENGTH | 0.813 INCHES NOMINAL IN |
| ENGINE SECTION LOCATION | COMPRESSOR |
| SPECIAL FEATURES | T.O. 2J-F100-4 FIG 130 IND 4; 2J-F100-14 FIG 136 IND 3 |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | ORIG NAME DISK,GAS TURBINE ENG |
| END ITEM IDENTIFICATION | ACFT ENG F100-PW-100/200 |
| MATERIAL | NICKEL ALLOY OVERALL |
No substitute or cross-reference records for this part.