Rotable Parts Exchange serves as a comprehensive source for military products, aerospace equipment, and Blade Turbine Rotor Aircraft Gas items. You have expressed particular interest in part number 301-330-113-0, a Cfm International Inc component we offer that is presented with the NSN 2840-01-466-7430 for straightforward identification and procurement. By completing and submitting the Request for Quote form provided on this page, you can obtain pricing details on this NSN part for your comparisons. Once our staff members receive and review your submitted information, a dedicated account manager will directly contact you with a response within 15 minutes or less.
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We strive to streamline the purchasing process and simplify it as much as possible, which includes providing detailed listings for all components to help customers pinpoint their exact needs. For instance, part number 301-330-113-0 is manufactured by Cfm International Inc under the CAGE Code 58828. Additionally, by using the initial digits of the NSN 2840-01-466-7430, you can discover that this component is associated with the FSC 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components. If you have any specific questions about our database, you may always give us a call or email, as we would be delighted to assist you however we can. Otherwise, we encourage you to secure a quote for part number 301-330-113-0 at your earliest convenience.
NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
2840-01-466-7430 Item PartTypeName: BLADE,TURBINE ROTOR,AIRCRAFT GAS | 2840 | 014667430 | 0 | N | ||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
7 | A | 0 | ||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
301-330-113-0 | 5 | 9 | 5 |
MRC | Criteria | Characteristic |
---|---|---|
ABHP | OVERALL LENGTH | 3.650 INCHES NOMINAL |
AGAV | END ITEM IDENTIFICATION | F108CF100 AND F108CF200 |
CRTL | CRITICALITY CODE JUSTIFICATION | AGAV |
CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | BLADE-LPT ROTOR STG 1 |
CZBJ | ENGINE SECTION LOCATION | LOW PRESSURE TURBINE |
CZCJ | STAGE NUMBER | 1 |
MATT | III MATERIAL | NICKEL ALLOY OVERALL |
RDAL | REFERENCE DATA AND LITERATURE | T.O. 2J-F108-14 FIG 9A IND 522C |
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