51566-6: CASE AND NOZZLE ASSEMBLY,TURBINE.
CASE AND NOZZLE ASSEMBLY,TURBINE. Key specifications include outside_diameter: 10.750 INCHES NOMINAL IN, mounting_hole_type: ROUND, UNTHREADED, raised_surface_height: 0.950 INCHES MINIMUM AND 0.952 INCHES MAXIMUM IN, mounting_hole_diameter: 0.688 INCHES NOMINAL IN, mounting_bolt_circle_diameter: 9.250 INCHES NOMINAL IN, mounting_hole_arrangement_style: SINGLE BOLT HOLE CIRCLE. This part is cataloged in the U.S.
Government catalog under NSN 2840-00-798-2846, 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.
| outside_diameter | 10.750 INCHES NOMINAL IN |
| mounting_hole_type | ROUND, UNTHREADED |
| raised_surface_height | 0.950 INCHES MINIMUM AND 0.952 INCHES MAXIMUM IN |
| mounting_hole_diameter | 0.688 INCHES NOMINAL IN |
| bolt_circle_hole_quantity | 6 |
| mounting_bolt_circle_diameter | 9.250 INCHES NOMINAL IN |
| mounting_hole_arrangement_style | SINGLE BOLT HOLE CIRCLE |
| general_characteristics_item_description | FOR 30 AWG WIRE; 0.038 IN. (0.97MM) TERMINAL HOLE DIA; 1 IN. (25.4MM) TERMINAL HOLE DEPTH; TWO-WAY STYLE; 4-1/4 IN. HANDLE LG; 7/8 IN. BIT LENGTH MM |
| NSN | 2840-00-798-2846 |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| ENGINE SECTION LOCATION | TURBINE |
| SPECIAL FEATURES | ORIGINAL NAME CASE AND NOZZLE,TURBINE,TURBINE ENGINE |
| END ITEM IDENTIFICATION | TF-33 AIRCRAFT ENGINE |
No substitute or cross-reference records for this part.