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 301-330-113-0, a Cfm International Inc item that is listed alongside the description “Blade Turbine Rotor Aircraft Gas” and the NSN 2840014667430. To guarantee a swift procurement process for NSN part number 301-330-113-0, 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 301-330-113-0 is manufactured by Cfm International Inc, it is specifically done so under CAGE Code 58828, 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 2840-01-466-7430, one can also determine that this part falls under FSC 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and 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 |
---|---|---|---|---|---|---|
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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