6539-11-165-2102: GEAR,SPUR.
The GEAR,SPUR is a the manufacturer industrial component. Key specifications include material: STEEL COMP E9310 OVERALL, body_style: PLAIN, WITH LIGHTENING HOLES, tooth_form: STANDARD, pressure_angle: 20.0000 DEGREES, teeth_quantity: 133, special_features: FLIGHT SAFETY CRITICAL. This part is cataloged in the U.S.
Government catalog under NSN 3020-01-130-2986, 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 | STEEL COMP E9310 OVERALL |
| body_style | PLAIN, WITH LIGHTENING HOLES |
| tooth_form | STANDARD |
| pressure_angle | 20.0000 DEGREES |
| teeth_quantity | 133 |
| special_features | FLIGHT SAFETY CRITICAL |
| attachment_method | MOUNTING HOLE |
| criticality_code_justification | FEAT |
| mounting_hole_type_and_quantity | 32 THREADED AXIALLY THROUGH BODY FIRST END |
| bolt_hole_circle_nominal_diameter | 7.631 INCHES AXIALLY THROUGH BODY FIRST END IN |
| material_document_and_classification | AMS 6260 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| mounting_hole_thread_quantity_per_inch | 24 AXIALLY THROUGH BODY FIRST END |
| NSN | 3020-01-130-2986 |
| TEETH QUANTITY | 133 |
| BODY STYLE | PLAIN, WITH LIGHTENING HOLES |
| MOUNTING HOLE TYPE AND QUANTITY | 32 THREADED AXIALLY THROUGH BODY FIRST END |
| CRITICALITY CODE JUSTIFICATION | FEAT |
| MATERIAL DOCUMENT AND CLASSIFICATION | AMS 6260 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| TOOTH FORM | STANDARD |
| MOUNTING HOLE THREAD QUANTITY PER INCH | 24 AXIALLY THROUGH BODY FIRST END |
| SPECIAL FEATURES | FLIGHT SAFETY CRITICAL |
| PRESSURE ANGLE | 20.0000 DEGREES |
| MATERIAL | STEEL COMP E9310 OVERALL |
No substitute or cross-reference records for this part.