734874-1: SHROUD SEGMENT,TURBINE,AIRCRAFT.
SHROUD SEGMENT,TURBINE,AIRCRAFT. Key specifications include diameter: 20.430 INCHES MINIMUM AND 20.450 INCHES MAXIMUM IN, material: STEEL OVERALL, overall_width: 1.138 INCHES MINIMUM AND 1.146 INCHES MAXIMUM IN, overall_length: 20.000 INCHES NOMINAL IN, special_features: TOLERANCE,FIT,FUNCTION, material_thickness: 2.000 INCHES NOMINAL IN. This part is cataloged in the U.S.
Government catalog under NSN 5310-00-734-8741, 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 | 20.430 INCHES MINIMUM AND 20.450 INCHES MAXIMUM IN |
| material | STEEL OVERALL |
| overall_width | 1.138 INCHES MINIMUM AND 1.146 INCHES MAXIMUM IN |
| overall_length | 20.000 INCHES NOMINAL IN |
| special_features | TOLERANCE,FIT,FUNCTION |
| material_thickness | 2.000 INCHES NOMINAL IN |
| end_item_identification | ACFT ENG TF33 |
| engine_section_location | TURBINE |
| criticality_code_justification | FEAT |
| NSN | 5310-00-734-8741 |
| OVERALL HEIGHT | 0.124 INCHES MINIMUM AND 0.127 INCHES MAXIMUM IN |
| SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | MIL-C-13924 CL 2 MIL SPEC SINGLE TREATMENT RESPONSE OVERALL |
| HEAT TREATMENT | QUENCHED AND TEMPERED |
| HARDNESS RATING | 43.0 ROCKWELL C MINIMUM AND 48.0 ROCKWELL C MAXIMUM |
| STYLE DESIGNATOR | SPRING TENSION |
| MATERIAL DOCUMENT AND CLASSIFICATION | SAE ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| OUTSIDE DIAMETER | 1.484 INCHES MINIMUM AND 1.516 INCHES MAXIMUM IN |
| MATERIAL THICKNESS | 0.059 INCHES MINIMUM AND 0.065 INCHES MAXIMUM IN |
| COLOR | BLACK OVERALL |
| SURFACE TREATMENT | OXIDE FILM OVERALL |