Thank you for your interest in 9547M14 available NSN part on NSN Sphere. Rotor Compressor Ai is listed with the part number 9547M14, and its manufacturer is General Electric Inc. This NSN part is currently available for purchase through our website today, and you may begin the process by filling out the following RFQ form. By providing us with information such as what parts you need, when you need them by, and your target price, our team can present you with a personalized quote that has been specifically tailored to fit your individual needs and requirements. Once you have submitted your request, a dedicated account manager will review and reach out to you in 15 minutes or less to continue the purchasing process.
As a leading online distributor of NSN parts like 9547M14, we provide customers access to an expansive database of new, used, and obsolete items that have been sourced from top global manufacturers such as General Electric Inc. If you are facing an AOG situation or time constraint, we provide same-day delivery and expedited shipping on a number of items. Get started on the purchasing process for NSN 2840014472505 under FSC 2840 Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components and experience how NSN Sphere can serve as your strategic sourcing partner for all of your operational needs.
NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
2840-01-447-2505 Item Description: Rotor Compressor Ai | 2840 | 014472505 | 0 | N | ||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
I | A | 0 | ||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
9547m14 | 3 | 9 | D |
MRC | Criteria | Characteristic |
---|---|---|
ABHP | OVERALL LENGTH | 25.577 INCHES MINIMUM AND 25.597 INCHES MAXIMUM |
AGAV | END ITEM IDENTIFICATION | F110-129 AIRCRAFT GAS TURBINE ENGINE |
APGF | DESIGN TYPE | AXIAL COMPRESSOR |
CRTL | CRITICALITY CODE JUSTIFICATION | FEAT AND CZBJ AND ABHP |
CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | ORIGINAL NAME ROTOR ASSEMBLY,COMPRESSOR |
CZBJ | ENGINE SECTION LOCATION | COMPRESSOR |
FEAT | SPECIAL FEATURES | 5INCLUDES STAGES 1-9; HPCR STG 1-2 HAS IMPROVED SPOOL OIL DRAIN HOLES (2) THAT ARE 1.48 TIME LARGER THAN THE CURRENT ELLIPTICAL HOLE; REPLACES P/N 9547M14G03 AND 9547M14G06; CHANGE OF HOLE IS A PHYSICAL CHANGE BUT NOT FUNCTIONALLY INTERCHAN |
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