4060952: NOZZLE SEGMENT,TURBINE,AIRCRAFT.
NOZZLE SEGMENT,TURBINE,AIRCRAFT. Key specifications include angle: 40.0 DEGREES, material: RUBBER CHLOROPRENE CLASS CR AND RUBBER NEOPRENE AND RUBBER SYNTHETIC OVERALL, nominal_width: 0.844 INCHES IN, style_designator: MULTI-RIB BAND DRIVE, nominal_effective_outside_length: 95.625 INCHES IN. This part is cataloged in the U.S.
Government catalog under NSN 2840-01-151-0373, 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.
| angle | 40.0 DEGREES |
| material | RUBBER CHLOROPRENE CLASS CR AND RUBBER NEOPRENE AND RUBBER SYNTHETIC OVERALL |
| nominal_width | 0.844 INCHES IN |
| section_quantity | 6 |
| style_designator | MULTI-RIB BAND DRIVE |
| nominal_effective_outside_length | 95.625 INCHES IN |
| NSN | 2840-01-151-0373 |
| STAGE NUMBER | 2 |
| DESIGN TYPE | AXIAL COMPRESSOR |
| CRITICALITY CODE JUSTIFICATION | FEAT |
| ENGINE SECTION LOCATION | TURBINE |
| SPECIAL FEATURES | T.O. 2J-F100-14, FIG 153, IND 22; 1800 CYCLE; 2.452-2.471 SQ. IN. AREA; REPLACED BY 4054752CLG |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | ORIGINAL NAME VANE,COMPRESSOR,AIRCRAFT GAS TURBINE ENGINE |
| END ITEM IDENTIFICATION | ACFT ENG F100/200 |
No substitute or cross-reference records for this part.