4082748-01: SEAL,AIR,AIRCRAFT GAS TURBINE EN.
SEAL,AIR,AIRCRAFT GAS TURBINE EN. Key specifications include diameter: 19.626 INCHES MINIMUM AND 19.630 INCHES MAXIMUM IN, material: NICKEL ALLOY OVERALL, design_type: AXIAL COMPRESSOR, overall_width: 0.258 INCHES MINIMUM AND 0.268 INCHES MAXIMUM IN, overall_length: 0.154 INCHES MINIMUM AND 0.166 INCHES MAXIMUM IN, end_item_identification: F100-PW-229 AIRCRAFT GAS TURBINE ENGINE. This part is cataloged in the U.S.
Government catalog under NSN 2840-01-448-7033, 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 | 19.626 INCHES MINIMUM AND 19.630 INCHES MAXIMUM IN |
| material | NICKEL ALLOY OVERALL |
| design_type | AXIAL COMPRESSOR |
| stage_number | 1 |
| overall_width | 0.258 INCHES MINIMUM AND 0.268 INCHES MAXIMUM IN |
| overall_length | 0.154 INCHES MINIMUM AND 0.166 INCHES MAXIMUM IN |
| end_item_identification | F100-PW-229 AIRCRAFT GAS TURBINE ENGINE |
| engine_section_location | COMBUSTION CHAMBER |
| criticality_code_justification | ABHP AND ABMZ AND ABMK AND CZBJ AND FEAT |
| material_document_and_classification | AMS5599 ASSN STD 1ST MATERIAL RESPONSE OR AMS5666 ASSN STD 2ND MATERIAL RESPONSE OVERALL |
| part_name_assigned_by_controlling_agency | ORIGINAL NAME BRUSHSEAL,INNER |
| NSN | 2840-01-448-7033 |
| STAGE NUMBER | 1 |
| DESIGN TYPE | AXIAL COMPRESSOR |
| CRITICALITY CODE JUSTIFICATION | ABHP AND ABMZ AND ABMK AND CZBJ AND FEAT |
| MATERIAL DOCUMENT AND CLASSIFICATION | AMS5599 ASSN STD 1ST MATERIAL RESPONSE OR AMS5666 ASSN STD 2ND MATERIAL RESPONSE OVERALL |
| DIAMETER | 19.626 INCHES MINIMUM AND 19.630 INCHES MAXIMUM IN |
| OVERALL LENGTH | 0.154 INCHES MINIMUM AND 0.166 INCHES MAXIMUM IN |
| OVERALL WIDTH | 0.258 INCHES MINIMUM AND 0.268 INCHES MAXIMUM IN |
| ENGINE SECTION LOCATION | COMBUSTION CHAMBER |
| SPECIAL FEATURES | T.O. 2J-F100-54, FIG 86, IND 19G; SEAL CONTAINS BRUSH WIRE PACK THAT HAS 2250-2650 WIRES PER CIRCUMFERENTIAL INCH; USE ONLY ON P/NS 4083194, 4083560 AND 4083565; LOCATED NEAR THE REAR COMPRESSOR DRIVE TURBINE ROTOR AND STATOR ASSY, TURBINE STATOR SUPPORT G |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | ORIGINAL NAME BRUSHSEAL,INNER |