Thank you for taking an interest in part number 9547M14, a General Electric Company product we have in stock that is listed alongside the NSN 2840014472505 and the description “Rotor Compressor Aircraft Gas Tu.” As part number 9547M14 is readily available for purchase on our website at any time, you are invited to fill out and submit the RFQ form provided on this page for the means of requesting a quote for your comparisons. All that we ask is that you supply us with important information such as your target price and expected shipping time frame so that we can best tailor a solution that caters to your unique needs and restrictions alike.
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To ensure that you only procure the exact items you require for carrying out operations, we list all aerospace parts, military and defense parts, and other product offerings with all applicable information for identification. For example, part number 9547M14 is listed alongside the NSN 2840-01-447-2505, meaning that it also belongs to FSC 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components. Furthermore, this NSN part is specifically manufactured under CAGE Code 07482, a unique identifier belonging to the manufacturer for a specific facility. With all of this in mind, kick off purchasing with us today and see why so many customers steadily choose us for their operational needs.
NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
2840-01-447-2505 Item PartTypeName: ROTOR,COMPRESSOR,AIRCRAFT GAS TU | 2840 | 014472505 | 0 | N | ||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
I | A | 0 | ||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
9547M14G08 | 1 | 2 | 3 |
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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