2840PL0712539: DUCT,COMPRESSOR,AIRCRAFT GAS TUR.
DUCT,COMPRESSOR,AIRCRAFT GAS TUR. Key specifications include diameter: 27.647 INCHES MINIMUM AND 27.659 INCHES MAXIMUM IN, material: NICKEL ALLOY DUCT, overall_width: 2.320 INCHES MINIMUM AND 2.326 INCHES MAXIMUM IN, overall_length: 12.130 INCHES NOMINAL IN, end_item_identification: F100-PW-229 AIRCRAFT GAS TURBINE ENGINE, engine_section_location: COMPRESSOR. This part is cataloged in the U.S.
Government catalog under NSN 2840-01-451-9636, 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 | 27.647 INCHES MINIMUM AND 27.659 INCHES MAXIMUM IN |
| material | NICKEL ALLOY DUCT |
| overall_width | 2.320 INCHES MINIMUM AND 2.326 INCHES MAXIMUM IN |
| overall_length | 12.130 INCHES NOMINAL IN |
| special_features | NO 3. BEARING REAL SEAL ASSY, REAR COMPRESSOR STATOR VARIABLE INLET VANES, EXIT FAN STATOR AND COMPRESSOR INTERMEDIATE CASE ASSY; STAGE 4; REPLACES P/N 4081682-01; CORROSION RESISTANT SEGMENTS |
| end_item_identification | F100-PW-229 AIRCRAFT GAS TURBINE ENGINE |
| engine_section_location | COMPRESSOR |
| reference_data_and_literature | T.O. 2J-F100-54, FIG 84, IND 16 AND 17 |
| criticality_code_justification | ABMK AND ABHP AND ABMZ AND FEAT |
| material_document_and_classification | AMS5771 ASSN STD SINGLE MATERIAL RESPONSE DUCT |
| part_name_assigned_by_controlling_agency | ORIGINAL NAME DUCT SEGMENT,COMPRESSOR |
| NSN | 2840-01-451-9636 |
| CRITICALITY CODE JUSTIFICATION | ABMK AND ABHP AND ABMZ AND FEAT |
| REFERENCE DATA AND LITERATURE | T.O. 2J-F100-54, FIG 84, IND 16 AND 17 |
| MATERIAL DOCUMENT AND CLASSIFICATION | AMS5771 ASSN STD SINGLE MATERIAL RESPONSE DUCT |
| DIAMETER | 27.647 INCHES MINIMUM AND 27.659 INCHES MAXIMUM IN |
| OVERALL LENGTH | 12.130 INCHES NOMINAL IN |
| OVERALL WIDTH | 2.320 INCHES MINIMUM AND 2.326 INCHES MAXIMUM IN |
| ENGINE SECTION LOCATION | COMPRESSOR |
| SPECIAL FEATURES | NO 3. BEARING REAL SEAL ASSY, REAR COMPRESSOR STATOR VARIABLE INLET VANES, EXIT FAN STATOR AND COMPRESSOR INTERMEDIATE CASE ASSY; STAGE 4; REPLACES P/N 4081682-01; CORROSION RESISTANT SEGMENTS |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | ORIGINAL NAME DUCT SEGMENT,COMPRESSOR |
| END ITEM IDENTIFICATION | F100-PW-229 AIRCRAFT GAS TURBINE ENGINE |