Whether you are in search of military and defense parts, aerospace parts, or other similar product solutions, Satellite To Submarine Parts is your one-stop shop. Thank you for your interest in part number X9241585-10, a Air Force United States Department item that is listed alongside the description “Crank Assembly Bell” and the NSN 1680013644094. To guarantee a swift procurement process for NSN part number X9241585-10, be sure to request a quote by filling out and submitting the RFQ form below, and one of our experts will offer a customized solution for your comparisons in response.
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We list everything with as much relevant information as possible to ensure that customers can swiftly identify and procure the exact products they need. For instance, while part number X9241585-10 is manufactured by Air Force United States Department, it is specifically done so under CAGE Code 98748, a unique identifier assigned to a particular facility by the DLA that supplies to various government or defense agencies. Additionally, using the first digits of the NSN 1680-01-364-4094, one can also determine that this part falls under FSC 1680 Miscellaneous Aircraft Accessories Components. Keeping this in mind, initiate the purchasing process today to see why so many customers depend on us for the NSN items they require.
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 1680-01-364-4094 Item PartTypeName: CRANK ASSEMBLY,BELL | 1680 | 013644094 | 0 | N | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| U | A | 0 | ||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| X9241585-10 | 5 | 2 | 3 |
| MRC | Criteria | Characteristic |
|---|---|---|
| AGAV | END ITEM IDENTIFICATION | B-1B AIRCRAFT |
| FEAT | SPECIAL FEATURES | INCLUDES 1 BUSHING; HEAT TREAT TO COND H1000; PER MIL-H-6875 |
| ZZZV | FSC APPLICATION DATA | UPLOCK ASSY,NOSE LANDING GEAR |
| TEXT | GENERAL CHARACTERISTICS ITEM DESCRIPTION | CRES BAR ALLOY PH13-8M0; PER AMS 5629; 2.250 IN. CENTER TO CENTER DISTANCE BETWEEN FULCRUM AND 1ST END ARM END HOLE; 0.375 IN. 1ST ARM END RADIUS; 2.745 IN. CENTER TO CENTER DISTANCE BETWEEN FULCRUM AND 2ND ARM END HOLE; 0.440 IN. 2ND ARM E |
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