901-236-009-133: PIN,GROOVED,HEADLESS.
The PIN,GROOVED,HEADLESS is a the manufacturer industrial component. Key specifications include diameter: 0.195 INCHES MINIMUM AND 2.000 INCHES MAXIMUM IN, material: STEEL OVERALL, overall_length: 1.750 INCHES NOMINAL IN, first_end_style: CHAMFERED, special_features: CONTRACTOR SUPPORTED ITEM FOR NAVICP PHIL CONSUMMABLE, MAIN LANDING GEAR TRUNION PIN, style_designator: CIRCULAR GROOVE. This part is cataloged in the U.S.
Government catalog under NSN 5315-01-517-0722, 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 | 0.195 INCHES MINIMUM AND 2.000 INCHES MAXIMUM IN |
| material | STEEL OVERALL |
| overall_length | 1.750 INCHES NOMINAL IN |
| first_end_style | CHAMFERED |
| special_features | CONTRACTOR SUPPORTED ITEM FOR NAVICP PHIL CONSUMMABLE, MAIN LANDING GEAR TRUNION PIN |
| style_designator | CIRCULAR GROOVE |
| first_end_location | CHAMFERED END |
| first_end_taper_angle | 45.0 DEGREES NOMINAL |
| first_end_taper_length | 0.030 INCHES NOMINAL IN |
| end_item_identification | MV-22 OSPREY TILT-ROTOR AIRCRAFT |
| criticality_code_justification | AGAV |
| material_document_and_classification | AMS 5862 ASSN STD SINGLE MATERIAL RESPONSE OR AMS 5659 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| NSN | 5315-01-517-0722 |
| FIRST END TAPER LENGTH | 0.030 INCHES NOMINAL IN |
| FIRST END LOCATION | CHAMFERED END |
| FIRST END STYLE | CHAMFERED |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| STYLE DESIGNATOR | CIRCULAR GROOVE |
| MATERIAL DOCUMENT AND CLASSIFICATION | AMS 5862 ASSN STD SINGLE MATERIAL RESPONSE OR AMS 5659 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| DIAMETER | 0.195 INCHES MINIMUM AND 2.000 INCHES MAXIMUM IN |
| OVERALL LENGTH | 1.750 INCHES NOMINAL IN |
| FIRST END TAPER ANGLE | 45.0 DEGREES NOMINAL |
| SECOND END RELATIONSHIP WITH FIRST END | IDENTICAL |
No substitute or cross-reference records for this part.