2110M32: LOCK RING,TURBINE NOZZLE,AIRCRAF.
LOCK RING,TURBINE NOZZLE,AIRCRAF. Key specifications include material: TITANIUM ALLOY, special_features: OVERALL WIDTH; 25 INCH IN, overall_thickness: 0.030 INCHES NOMINAL IN, end_item_identification: ENGINE, F101-GE-100 (B1), material_document_and_classification: AMS 4911 ASSN STD SINGLE MATERIAL RESPONSE, part_name_assigned_by_controlling_agency: RING, SUPPORT LINER, NOZZLE. This part is cataloged in the U.S.
Government catalog under NSN 2840-01-482-2473, 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.
| material | TITANIUM ALLOY |
| special_features | OVERALL WIDTH; 25 INCH IN |
| overall_thickness | 0.030 INCHES NOMINAL IN |
| end_item_identification | ENGINE, F101-GE-100 (B1) |
| material_document_and_classification | AMS 4911 ASSN STD SINGLE MATERIAL RESPONSE |
| part_name_assigned_by_controlling_agency | RING, SUPPORT LINER, NOZZLE |
| NSN | 2840-01-482-2473 |
| OVERALL THICKNESS | 0.030 INCHES NOMINAL IN |
| MATERIAL DOCUMENT AND CLASSIFICATION | AMS 4911 ASSN STD SINGLE MATERIAL RESPONSE |
| SPECIAL FEATURES | OVERALL WIDTH; 25 INCH IN |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | RING, SUPPORT LINER, NOZZLE |
| END ITEM IDENTIFICATION | ENGINE, F101-GE-100 (B1) |
| MATERIAL | TITANIUM ALLOY |
No substitute or cross-reference records for this part.