Nuts and Washers: MS21060L08, MS21061-04, MS21061-4
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| MS21060L08 | 5310-00-779-6737 | Nut, Self-Locking, Plate | Material: Iron alloy 660 overall Material Document AND Classification: Ams 5525 assn std single material response overall or ams 5735 assn std single material response overall or ams 5737 assn std single material response overall Surface Treatment: Passivate overall | Military Standards (96906) National Aerospace Standards (80205) | |
| MS21060L08K | 5310-00-779-6736 | Nut, Self-Locking, Plate | Material: Iron alloy 660 overall Material Document and Classification: Ams 5525 assn std single material response or ams 5735 assn std single material response or ams 5737 assn std single material response overall Surface Treatment: Passivate overall | Military Standards (96906) National Aerospace Standards (80205) | |
| MS21060L3 | 5310-00-779-6625 | Nut, Self-Locking, Plate | Thread Class: 3B Thread Direction: Right-hand Locking Feature: Prevailing torque all metal design | Bosch Rexroth GMBH Lohmann (D9182) Columbia Nut & Bolt LLC (51792) Military Standards (96906) National Aerospace Standards (80205) | |
| MS21060L3 | 5310-01-497-4173 | Nut, Self-Locking, Plate | Material: Iron alloy 660 overall Material Document and Classification: Ams 5735 assn std single material response or ams 5737 assn std single material response or ams 5525 assn std single material response overall Surface Treatment: Passivate overall | Rolls Royce Corp. (1E0F1) | |
| MS21060L3K | 5310-00-779-6735 | Nut, Self-Locking, Plate | Material: Iron alloy 660 overall Material Document and Classification: Ams 5525 assn std single material response or ams 5735 assn std single material response or ams 5737 assn std single material response overall Surface Treatment: Passivate overall | Military Standards (96906) National Aerospace Standards (80205) | |
| MS21060L3W | 5310-01-189-6515 | Nut, Self-Locking, Plate | Material: Iron alloy 660 overall Material Document and Classification: Ams 5525 assn std single material response or ams 5732 assn std single material response or ams 5737 assn std single material response overall Hardness Rating: 49.0 rockwell C maximum | Military Standards (96906) | |
| MS21060L4 | 5310-00-779-6689 | Nut, Self-Locking, Plate | Material: Iron alloy 660 overall Material Document AND Classification: Ams 5525 assn std single material response overall or ams 5735 assn std single material response overall or ams 5737 assn std single material response overall Surface Treatment: Passivate overall | Military Standards (96906) National Aerospace Standards (80205) | |
| MS21060L4K | 5310-00-779-6651 | Nut, Self-Locking, Plate | Material: Iron alloy 660 overall Material Document and Classification: Ams 5525 assn std single material response or ams 5735 assn std single material response or ams 5737 assn std single material response overall Surface Treatment: Passivate overall | Military Standards (96906) | |
| MS21060L5 | 5310-00-779-6636 | Nut, Self-Locking, Plate | Material: Iron alloy 660 overall Material Document AND Classification: Ams 5732 assn std single material response overall or ams 5737 assn std single material response overall or ams 5525 assn std single material response overall Surface Treatment: Passivate overall | Military Standards (96906) National Aerospace Standards (80205) | |
| MS21060L5K | 5310-01-056-3540 | Nut, Self-Locking, Plate | Material: Iron alloy 660 overall Surface Treatment: Passivate overall Hardness Rating: 49.0 rockwell C maximum | Military Standards (96906) Society of Automotive Engineers Inc. (81343) | |
| MS21060L6 | 5310-00-779-6633 | Nut, Self-Locking, Plate | Material: Iron alloy 660 overall Material Document AND Classification: Ams 5735 assn std single material response overall or ams 5737 assn std single material response overall or ams 5525 assn std single material response overall Surface Treatment: Passivate overall | Military Standards (96906) National Aerospace Standards (80205) | |
| MS21060L7 | 5310-01-529-6740 | Nut, Self-Locking, Plate | Material: Iron alloy 660 overall Material Document and Classification: Ams 5525 assn std single material response or ams 5732 assn std single material response or ams 5737 assn std single material response overall Hardness Rating: 49.0 rockwell C maximum | Military Standards (96906) National Aerospace Standards (80205) | |
| MS21060-L8 MS21060L8 | 5310-01-481-7120 | Nut, Self-Locking, Plate | Material: Iron alloy 660 overall Material Document and Classification: Ams 5525 assn std 1ST material response or ams 5732 assn std 2ND material response or ams 5737; (uns S66286) assn std 3RD material response overall Hardness Rating: 49.0 rockwell C maximum | Military Standards (96906) National Aerospace Standards (80205) | |
| MS21061-04 MS2106104 | 5310-00-339-8558 | Nut, Self-Locking, Plate | Material: Steel overall Surface Treatment: Cadmium overall Hardness Rating: 49.0 rockwell C maximum | Military Standards (96906) National Aerospace Standards (80205) | |
| MS21061-06 MS2106106 | 5310-00-778-9461 | Nut, Self-Locking, Plate | Material: Steel overall Surface Treatment: Cadmium overall Hardness Rating: 49.0 rockwell C maximum | Military Standards (96906) National Aerospace Standards (80205) | |
| MS21061-06K MS2106106K | 5310-01-337-9135 | Nut, Self-Locking, Plate | Material: Steel overall Surface Treatment: Cadmium or chromate overall Hardness Rating: 49.0 rockwell C maximum | Military Standards (96906) National Aerospace Standards (80205) | |
| MS21061-08 MS2106108 | 5310-00-778-9476 | Nut, Self-Locking, Plate | Material: Steel overall Surface Treatment: Cadmium overall Hardness Rating: 49.0 rockwell C maximum | Military Standards (96906) National Aerospace Standards (80205) | |
| MS21061-08K MS2106108K | 5310-01-124-7710 | Nut, Self-Locking, Plate | Material: Steel overall Surface Treatment: Cadmium and chromate overall Hardness Rating: 49.0 rockwell C maximum | Military Standards (96906) National Aerospace Standards (80205) | |
| MS21061-3 MS210613 | 5310-00-778-9285 | Nut, Self-Locking, Plate | Thread Class: 3B Thread Direction: Right-hand Locking Feature: Prevailing torque all metal design | Military Standards (96906) National Aerospace Standards (80205) | |
| MS21061-3K MS210613K | 5310-00-778-9291 | Nut, Self-Locking, Plate | Material: Steel overall Surface Treatment: Cadmium overall Hardness Rating: 49.0 rockwell C maximum | Military Standards (96906) National Aerospace Standards (80205) | |
| MS21061-4 MS210614 | 5310-00-778-9283 | Nut, Self-Locking, Plate | Material: Steel overall Surface Treatment: Cadmium overall Hardness Rating: 49.0 rockwell C maximum | Military Standards (96906) National Aerospace Standards (80205) |