1168857-1: PIN,GROOVED,HEADLESS.
The PIN,GROOVED,HEADLESS is a the manufacturer industrial component. Key specifications include diameter: 0.249 INCHES MINIMUM AND 0.250 INCHES MAXIMUM IN, material: STEEL COMP XM-12 OVERALL, overall_length: 1.170 INCHES NOMINAL IN, effective_length: 1.010 INCHES NOMINAL IN, special_features: HEAT TREATMENT, ANNEALED AND TEMPERED., style_designator: GROOVE. This part is cataloged in the U.S.
Government catalog under NSN 5315-01-163-9554, 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 | 0.249 INCHES MINIMUM AND 0.250 INCHES MAXIMUM IN |
| material | STEEL COMP XM-12 OVERALL |
| overall_length | 1.170 INCHES NOMINAL IN |
| effective_length | 1.010 INCHES NOMINAL IN |
| special_features | HEAT TREATMENT, ANNEALED AND TEMPERED. |
| style_designator | GROOVE |
| undercut_diameter | 0.228 INCHES MINIMUM AND 0.231 INCHES MAXIMUM IN |
| end_item_identification | AH-64 HELICOPTER |
| nondefinitive_spec/std_data | H1025 PER AMS-H-6875 CONDITION |
| material_document_and_classification | AMS 5659 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| part_name_assigned_by_controlling_agency | PIN, GROOVED, HEADLESS, WHEEL LOCK, TAIL LANDING GEAR |
| NSN | 5315-01-163-9554 |
| UNDERCUT DIAMETER | 0.228 INCHES MINIMUM AND 0.231 INCHES MAXIMUM IN |
| STYLE DESIGNATOR | GROOVE |
| MATERIAL DOCUMENT AND CLASSIFICATION | AMS 5659 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| DIAMETER | 0.249 INCHES MINIMUM AND 0.250 INCHES MAXIMUM IN |
| OVERALL LENGTH | 1.170 INCHES NOMINAL IN |
| EFFECTIVE LENGTH | 1.010 INCHES NOMINAL IN |
| NONDEFINITIVE SPEC/STD DATA | H1025 PER AMS-H-6875 CONDITION |
| SPECIAL FEATURES | HEAT TREATMENT, ANNEALED AND TEMPERED. |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | PIN, GROOVED, HEADLESS, WHEEL LOCK, TAIL LANDING GEAR |
| END ITEM IDENTIFICATION | AH-64 HELICOPTER |
No substitute or cross-reference records for this part.