3014804: ROTOR,TURBINE,AIRCRAFT GAS TURBI.
ROTOR,TURBINE,AIRCRAFT GAS TURBI. Key specifications include material: NICKEL ALLOY OVERALL, overall_length: 3.945 INCHES MINIMUM AND 3.960 INCHES MAXIMUM IN, material_document_and_classification: CRES,CPW203 CAGE 00198 MFR REF SINGLE MATERIAL RESPONSE OVERALL. This part is cataloged in the U.S.
Government catalog under NSN 2840-00-157-3605, 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 | NICKEL ALLOY OVERALL |
| overall_length | 3.945 INCHES MINIMUM AND 3.960 INCHES MAXIMUM IN |
| material_document_and_classification | CRES,CPW203 CAGE 00198 MFR REF SINGLE MATERIAL RESPONSE OVERALL |
| NSN | 2840-00-157-3605 |
| MATERIAL DOCUMENT AND CLASSIFICATION | CRES,CPW203 CAGE 00198 MFR REF SINGLE MATERIAL RESPONSE OVERALL |
| OVERALL LENGTH | 3.945 INCHES MINIMUM AND 3.960 INCHES MAXIMUM IN |
| SPECIAL FEATURES | 58 BLADES; 8.547 MIN 8.549 MAX IN. O/A OD; 1ST END STEPPED HUB; 1.12 MIN 1.1207 MAX OD 1ST STEP 1ST END; 0.2 MIN 0.21 MAX LG 1ST STEP 1ST END; EXT SPLINES 2ND STEP 1ST END; 38 TEETH; 30 DEG PRESSURE ANGLE; 1.2188 IN. NOM PITCH DIA 0.54 MIN 0.57 MAX IN. LG 2ND STEP 1ST END; 1.11 MIN 1.13 MAX OD 3RD STEP 1ST END; 0.07 MIN 0.08 MAX IN. LG 3RD STEP 1ST END; 1.3 MIN 1.3007 MAX IN. OD 4TH STEP 1ST END; 0.155 MIN 0.16 MAX IN. LG 4TH STEP 1ST END; 1.82 MIN 1.83 MAX IN. OD 5TH STEP 1ST END; 6TH STEP 1ST END TAPERED:1.675 MIN 1. 685 MAX SMALLEST OD; 0.635 MIN 0.705 MAX IN. LG 6TH STEP 1ST END; 1.77 MIN 1.825 MAX LG FROM 1ST END TO DISK; 2ND END PLAIN HUB; 1.408 MIN. 1.412 MAX IN. OD HUB 2ND END ; 0.495 MIN 0.515 MAX IN. LG FROM 2ND END TO DISK; 4 HOLES 0.208 MIN 0.212 MAX IN. DIA; 0.125 MIN 0.145 MAX IN. LG 5TH STEP 1ST END IN |
| MATERIAL | NICKEL ALLOY OVERALL |
No substitute or cross-reference records for this part.