1864M44P001A: PLATE,COMPONENT MOUNTING,AIRCRAF.
PLATE,COMPONENT MOUNTING,AIRCRAF. Key specifications include special_features: MATL; B50TF25 CL-A (HAST X);HIGH PRESSURE TURBINE N0ZZLE STAGE 2, material_thickness: 0.018 INCHES MINIMUM AND 0.022 INCHES MAXIMUM IN, end_item_identification: TF-39 ENGINE, engine_section_location: TURBINE. This part is cataloged in the U.S.
Government catalog under NSN 2840-01-496-1184, 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.
| special_features | MATL; B50TF25 CL-A (HAST X);HIGH PRESSURE TURBINE N0ZZLE STAGE 2 |
| material_thickness | 0.018 INCHES MINIMUM AND 0.022 INCHES MAXIMUM IN |
| end_item_identification | TF-39 ENGINE |
| engine_section_location | TURBINE |
| NSN | 2840-01-496-1184 |
| ENGINE SECTION LOCATION | TURBINE |
| MATERIAL THICKNESS | 0.018 INCHES MINIMUM AND 0.022 INCHES MAXIMUM IN |
| SPECIAL FEATURES | MATL; B50TF25 CL-A (HAST X);HIGH PRESSURE TURBINE N0ZZLE STAGE 2 |
| END ITEM IDENTIFICATION | TF-39 ENGINE |
No substitute or cross-reference records for this part.