CA22051-6T22-19: SCREW ASSEMBLY,PANEL.
The SCREW ASSEMBLY,PANEL is a the manufacturer industrial component. Key specifications include material: NICKEL ALLOY 718 OVERALL, head_style: HEXAGON, head_height: 0.188 INCHES MINIMUM AND 0.209 INCHES MAXIMUM IN, thread_class: 3A A, fastener_length: 1.178 INCHES MINIMUM AND 1.198 INCHES MAXIMUM IN, thread_direction: RIGHT-HAND. This part is cataloged in the U.S.
Government catalog under NSN 5305-01-490-2960, 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 718 OVERALL |
| head_style | HEXAGON |
| head_height | 0.188 INCHES MINIMUM AND 0.209 INCHES MAXIMUM IN |
| thread_class | 3A A |
| fastener_length | 1.178 INCHES MINIMUM AND 1.198 INCHES MAXIMUM IN |
| thread_direction | RIGHT-HAND |
| width_between_flats | 0.554 INCHES MINIMUM AND 0.564 INCHES MAXIMUM IN |
| internal_drive_style | TORX |
| end_item_identification | F-22 RAPTOR |
| nominal_thread_diameter | 0.375 INCHES IN |
| thread_quantity_per_inch | 24 |
| thread_series_designator | UNIFIED NATIONAL JOINT FINE (UNJF) |
| NSN | 5305-01-490-2960 |
| HEAD HEIGHT | 0.188 INCHES MINIMUM AND 0.209 INCHES MAXIMUM IN |
| FASTENER LENGTH | 1.178 INCHES MINIMUM AND 1.198 INCHES MAXIMUM IN |
| MATERIAL ACCOMMODATED THICKNESS | 0.688 INCHES NOMINAL IN |
| NOMINAL THREAD DIAMETER | 0.375 INCHES IN |
| HEAD STYLE | HEXAGON |
| THREAD DIRECTION | RIGHT-HAND |
| WIDTH BETWEEN FLATS | 0.554 INCHES MINIMUM AND 0.564 INCHES MAXIMUM IN |
| INTERNAL DRIVE STYLE | TORX |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | SCREW |
| THREAD CLASS | 3A A |
No substitute or cross-reference records for this part.