Thank you for taking interest in Hamilton Sundstrand Corporation part number 552390, which is listed with the NSN 2915-00-797-4170 and a product description of “Retainer And Ball L.” In order to receive procurement options on this particular listing, we ask that you fill out and submit the form provided below with as much information as you can concerning your needs. By supplying our staff with key details on your desired quantity, pricing target, and expedited fulfillment timeframe, we can respond with a quote that has been specifically tailored to your unique specifications. We also ask that you make us aware of any restrictions that you may have as soon as possible, such as if you have a time constraint or are seeking unlisted items.
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Alongside part number 552390, you are encouraged to continue exploring our collection curated catalogs to find additional items that can accompany this Retainer And Ball L part with the NSN 2915-00-797-4170. For example, you can browse other Hamilton Sundstrand Corporation components that were produced under CAGE Code 73030 or listings that belong to FSC 2915 Engine Fuel System Components Aircraft and Missile Prime Movers with ease on our website, with search tools provided for quick location. Furthermore, our staff is just a call or email away from assisting you with any inquiries or requests, so be sure to get started on the quotation process for part number 552390 and other desired offerings on Aerospace Spare.
NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
2915-00-797-4170 Item PartTypeName: RETAINER AND BALL,L | 2915 | 007974170 | 0 | N | ||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
U | U | |||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
552390 | 6 | 9 | 5 |
MRC | Criteria | Characteristic |
---|---|---|
ADAV | OVERALL DIAMETER | 0.308 INCHES MAXIMUM |
CRTL | CRITICALITY CODE JUSTIFICATION | FEAT |
CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | RETAINER AND BALL-LINKAGE |
FEAT | SPECIAL FEATURES | CRITICAL SAFETY ITEM (CSI) |
SUPP | SUPPLEMENTARY FEATURES | NO CRACKS SHALL BE VISIBLE AT LIP UNDER 5X MAGNIFICATION AFTER SPINNING AND AFTER MEETING REQUIREMENTS OF HS4524 |
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