9523M58P01: SHIELD,HEAT,AIRCRAFT GAS TURBINE.
SHIELD,HEAT,AIRCRAFT GAS TURBINE. Key specifications include diameter: 16.360 INCHES MINIMUM AND 16.380 INCHES MAXIMUM IN, overall_length: 2.230 INCHES MINIMUM AND 2.250 INCHES MAXIMUM IN, special_features: MATL B50TF14 CL-A (INCO 718), material_thickness: 0.028 INCHES MINIMUM AND 0.036 INCHES MAXIMUM IN, end_item_identification: F108 AIRCRAFT ENGINE, engine_section_location: TURBINE. This part is cataloged in the U.S.
Government catalog under NSN 2840-01-187-8261, 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 | 16.360 INCHES MINIMUM AND 16.380 INCHES MAXIMUM IN |
| overall_length | 2.230 INCHES MINIMUM AND 2.250 INCHES MAXIMUM IN |
| special_features | MATL B50TF14 CL-A (INCO 718) |
| material_thickness | 0.028 INCHES MINIMUM AND 0.036 INCHES MAXIMUM IN |
| end_item_identification | F108 AIRCRAFT ENGINE |
| engine_section_location | TURBINE |
| criticality_code_justification | AGAV |
| NSN | 2840-01-187-8261 |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| DIAMETER | 16.360 INCHES MINIMUM AND 16.380 INCHES MAXIMUM IN |
| OVERALL LENGTH | 2.230 INCHES MINIMUM AND 2.250 INCHES MAXIMUM IN |
| ENGINE SECTION LOCATION | TURBINE |
| MATERIAL THICKNESS | 0.028 INCHES MINIMUM AND 0.036 INCHES MAXIMUM IN |
| SPECIAL FEATURES | MATL B50TF14 CL-A (INCO 718) |
| END ITEM IDENTIFICATION | F108 AIRCRAFT ENGINE |
No substitute or cross-reference records for this part.