4056162: CASE,COMPRESSOR,AIRCRAFT GAS TUR.
CASE,COMPRESSOR,AIRCRAFT GAS TUR. Key specifications include diameter: 23.130 INCHES MINIMUM AND 23.150 INCHES MAXIMUM IN, design_type: AXIAL COMPRESSOR, overall_length: 8.594 INCHES MINIMUM AND 8.598 INCHES MAXIMUM IN, hardness_rating: 36.0 ROCKWELL C NOMINAL OVERALL, special_features: T.O. 2J-F100-14, FIG 140, IND 9A;INCLUDES STAGES 10-13 A, fsc_application_data: F15 ACFT.
This part is cataloged in the U.S. Government catalog under NSN 2840-01-112-3783, 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 | 23.130 INCHES MINIMUM AND 23.150 INCHES MAXIMUM IN |
| design_type | AXIAL COMPRESSOR |
| overall_length | 8.594 INCHES MINIMUM AND 8.598 INCHES MAXIMUM IN |
| hardness_rating | 36.0 ROCKWELL C NOMINAL OVERALL |
| special_features | T.O. 2J-F100-14, FIG 140, IND 9A;INCLUDES STAGES 10-13 A |
| fsc_application_data | F15 ACFT |
| end_item_identification | ACFT ENG F100 |
| engine_section_location | COMPRESSOR |
| part_name_assigned_by_controlling_agency | CASE,AXIAL COMPRESSOR,TURBINE ENGINE |
| NSN | 2840-01-112-3783 |
| FSC APPLICATION DATA | F15 ACFT |
| DESIGN TYPE | AXIAL COMPRESSOR |
| HARDNESS RATING | 36.0 ROCKWELL C NOMINAL OVERALL |
| DIAMETER | 23.130 INCHES MINIMUM AND 23.150 INCHES MAXIMUM IN |
| OVERALL LENGTH | 8.594 INCHES MINIMUM AND 8.598 INCHES MAXIMUM IN |
| ENGINE SECTION LOCATION | COMPRESSOR |
| SPECIAL FEATURES | T.O. 2J-F100-14, FIG 140, IND 9A;INCLUDES STAGES 10-13 A |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | CASE,AXIAL COMPRESSOR,TURBINE ENGINE |
| END ITEM IDENTIFICATION | ACFT ENG F100 |
No substitute or cross-reference records for this part.