You are currently exploring our in-stock options for part number A51M42508-11 with the NSN 1680000050125. This product is listed with the description “Bell Crank” and is manufactured by Northrop Grumman Systems Corporation. If you are looking to purchase this part, we encourage you to complete and submit the RFQ form below with as much information as you can provide, such as your desired quantity, budget, shipping time frame, and more. Within 15 minutes of receiving and reviewing your submission, one of our experts will reach out with a quote that is tailored to your needs.
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We supply all relevant information alongside the listings on our website, that way you know you are always getting the exact item you require. For example, part number A51M42508-11 is listed alongside the NSN 1680-00-005-0125 and belongs to the FSC 1680 Miscellaneous Aircraft Accessories Components. Additionally, it is also under the CAGE Code 79RG9, which is assigned to Northrop Grumman Systems Corporation. At Aerospace Procurement, you can trust that each product in our inventory is up to industry standards, as we are committed to various quality assurance practices. For example, we uphold a strict NO CHINA SOURCING pledge to ensure that each part is shipped out alongside its manufacturer trace documentation and qualifying certifications. These practices and more allow us to operate with AS9120B, ISO 9001:2015, and FAA AC 00-56B accreditation. Get in contact with us today to see how we can make the procurement process for part number A51M42508-11 seamless.
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 1680-00-005-0125 Item PartTypeName: BELL CRANK | 1680 | 000050125 | 0 | N | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| U | A | 0 | ||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| A51M42508-11 | 2 | 2 | 3 |
| MRC | Criteria | Characteristic |
|---|---|---|
| ABXV | BORE DIAMETER | 0.500 INCHES MINIMUM AND 0.501 INCHES MAXIMUM |
| ADGE | BORE LENGTH | 1.457 INCHES MINIMUM AND 1.463 INCHES MAXIMUM |
| AGAV | END ITEM IDENTIFICATION | F-14 AIRCRAFT |
| CZLM | CENTER TO CENTER DISTANCE BETWEEN FULCRUM AND ARM END HOLE/SLOT/BALL | 1.427 INCHES NOMINAL 1ST END AND 1.432 INCHES MAXIMUM 1ST END |
| CZLM | CENTER TO CENTER DISTANCE BETWEEN FULCRUM AND ARM END HOLE/SLOT/BALL | 1.496 INCHES MINIMUM 2ND END AND 1.501 INCHES MAXIMUM 2ND END |
| CZLN | END HOLE/BALL DIAMETER | 0.249 INCHES MINIMUM 1ST END AND 0.251 INCHES MAXIMUM 1ST END |
| CZLN | END HOLE/BALL DIAMETER | 0.249 INCHES MINIMUM 2ND END AND 0.251 INCHES MAXIMUM 2ND END |
| MATT | MATERIAL | TITANIUM |
| STYL | STYLE DESIGNATOR | RAISED FACE PIVOT HOLE,CLEVIS BOTH ENDS |
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