4043279CL2: SEAL,AIR,AIRCRAFT GAS TURBINE EN.
SEAL,AIR,AIRCRAFT GAS TURBINE EN. Key specifications include diameter: 16.310 INCHES MINIMUM AND 16.330 INCHES MAXIMUM IN, material: NICKEL ALLOY OVERALL, design_type: AXIAL COMPRESSOR, stage_number: 10, overall_length: 1.705 INCHES MINIMUM AND 1.729 INCHES MAXIMUM IN, special_features: T.O. 2J-F100-14, FIG 138, IND 2.
This part is cataloged in the U.S. Government catalog under NSN 2840-00-395-7201, 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 | 16.310 INCHES MINIMUM AND 16.330 INCHES MAXIMUM IN |
| material | NICKEL ALLOY OVERALL |
| design_type | AXIAL COMPRESSOR |
| stage_number | 10 |
| overall_length | 1.705 INCHES MINIMUM AND 1.729 INCHES MAXIMUM IN |
| special_features | T.O. 2J-F100-14, FIG 138, IND 2 |
| fsc_application_data | F15 ACFT |
| end_item_identification | F-100 AIRCRAFT ENGINE |
| engine_section_location | COMPRESSOR |
| part_name_assigned_by_controlling_agency | SEAL,COMPRESSOR |
| NSN | 2840-00-395-7201 |
| FSC APPLICATION DATA | F15 ACFT |
| STAGE NUMBER | 10 |
| DESIGN TYPE | AXIAL COMPRESSOR |
| DIAMETER | 16.310 INCHES MINIMUM AND 16.330 INCHES MAXIMUM IN |
| OVERALL LENGTH | 1.705 INCHES MINIMUM AND 1.729 INCHES MAXIMUM IN |
| ENGINE SECTION LOCATION | COMPRESSOR |
| SPECIAL FEATURES | T.O. 2J-F100-14, FIG 138, IND 2 |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | SEAL,COMPRESSOR |
| END ITEM IDENTIFICATION | F-100 AIRCRAFT ENGINE |
| MATERIAL | NICKEL ALLOY OVERALL |
No substitute or cross-reference records for this part.