350-0432: CAP,ENGINE SHOCK MOUNT COOLING.
The CAP,ENGINE SHOCK MOUNT COOLING is a the manufacturer thermal management component critical for maintaining optimal operating temperatures in enterprise hardware. Key specifications include width: 0.125 INCHES NOMINAL IN, material: STEEL CORROSION RESISTING, wall_thickness: 0.016 INCHES NOMINAL IN, special_features: MEDIUM MINI-DIAMOND TWIN; THIN BASE; FOR MANDIBULAR RIGHT CUSPIDS USING LEVEL ARCH MODERN TECHNIQUE, part_name_assigned_by_controlling_agency: BRACKET ORTHODONTIC CRS0.016" THK 0.125" W F/MANDIBULAR R CUSPID. This part is cataloged in the U.S.
Government catalog under NSN 1560-00-331-4589, 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.
| width | 0.125 INCHES NOMINAL IN |
| material | STEEL CORROSION RESISTING |
| wall_thickness | 0.016 INCHES NOMINAL IN |
| special_features | MEDIUM MINI-DIAMOND TWIN; THIN BASE; FOR MANDIBULAR RIGHT CUSPIDS USING LEVEL ARCH MODERN TECHNIQUE |
| part_name_assigned_by_controlling_agency | BRACKET ORTHODONTIC CRS0.016" THK 0.125" W F/MANDIBULAR R CUSPID |
| NSN | 1560-00-331-4589 |
| END ITEM IDENTIFICATION | AIRCRAFT MODEL C118 |
No substitute or cross-reference records for this part.