Aerospace Performance Parts is pleased to offer immediate purchasing options for Cfm International Inc part number 301-330-114-0, which you have taken interest in. This Blade Turbine Rotor Aircraft Gas item is listed alongside the NSN 2840-01-466-7430 for ease of identification, with various additional information provided on this page for your reference. Should you wish to obtain solutions on this particular listing, we invite you to complete the Request for Quote (RFQ) form on this page at your earliest convenience. Responses are always offered shortly after we receive and review each request, with solutions we give being fully based on the details we are provided.
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If you happen to require expedited shipping for part number 301-330-114-0 or any other FSC 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components components we carry from Cfm International Inc under CAGE Code 58828, be sure to let us know as soon as possible. We would be happy to discuss the options that we can potentially provide, our track record of on-time delivery being a testament to our dedication to customer satisfaction. You can either include such details within your request, or get in touch with staff directly. Otherwise, request a quote on NSN 2840-01-466-7430 part number 301-330-114-0 today, knowing we will support all your operational needs with care.
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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