1964M15G05: AUGMENTOR NOZZLE SECTION,INNER,A.
AUGMENTOR NOZZLE SECTION,INNER,A. Key specifications include diameter: 24.115 INCHES MINIMUM AND 24.125 INCHES MAXIMUM IN, material: NICKEL ALLOY, design_type: AXIAL COMPRESSOR, overall_width: 0.658 INCHES NOMINAL IN, overall_length: 1.115 INCHES MINIMUM AND 1.145 INCHES MAXIMUM IN, inside_diameter: 13.648 INCHES MINIMUM AND 13.652 INCHES MAXIMUM IN. This part is cataloged in the U.S.
Government catalog under NSN 2840-01-499-6524, 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 | 24.115 INCHES MINIMUM AND 24.125 INCHES MAXIMUM IN |
| material | NICKEL ALLOY |
| design_type | AXIAL COMPRESSOR |
| stage_number | 1 |
| overall_width | 0.658 INCHES NOMINAL IN |
| overall_length | 1.115 INCHES MINIMUM AND 1.145 INCHES MAXIMUM IN |
| inside_diameter | 13.648 INCHES MINIMUM AND 13.652 INCHES MAXIMUM IN |
| outside_diameter | 21.950 INCHES MINIMUM AND 21.970 INCHES MAXIMUM IN |
| special_features | RETAINER FOR THE LOW PRESSURE TURBINE ROTOR, STAGE 1 |
| material_thickness | 0.074 INCHES MINIMUM AND 0.083 INCHES MAXIMUM IN |
| fsc_application_data | F110GE129 ENGINE |
| mounting_hole_diameter | 0.419 INCHES MINIMUM AND 0.430 INCHES MAXIMUM IN |
| NSN | 2840-01-499-6524 |