Thank you for taking an interest in part number 1461M87G15, a General Electric Company product we have in stock that is listed alongside the NSN 2840014608957 and the description “Frame Turbine Aircraft Gas Turbi.” As part number 1461M87G15 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 1461M87G15 is listed alongside the NSN 2840-01-460-8957, 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 |
---|---|---|---|---|---|---|
2840-01-460-8957 Item PartTypeName: FRAME,TURBINE,AIRCRAFT GAS TURBI | 2840 | 014608957 | 0 | N | ||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
I | A | 0 | ||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
1461M87G15 | 1 | 2 | 3 |
MRC | Criteria | Characteristic |
---|---|---|
ABKV | OUTSIDE DIAMETER | 33.556 INCHES NOMINAL |
AGAV | END ITEM IDENTIFICATION | F110-GE-129 ACFT GAS TURBINE ENG |
CZLB | NUMBER OF VARIABLE GUIDE VANES | 10 |
FEAT | SPECIAL FEATURES | THIS CHANGE ADDRESSES CRACKS AND RIVET BREAKAGE IN THE TURBINE FRAME FWD OUTER LINER SUPPORTS; ROOT CAUSE IS A LACK OF THERMAL GROWTH CAPABILITY,WHICH CAUSES THE SUPPORT TO CRACK AND LOAD THE RIVETS. CHANGES WILL INCREASE SHEET METAL HOLE S |
RDAL | REFERENCE DATA AND LITERATURE | T.O. 2J-F110-4, FIG 79, IND 15 ORFIG 81, IND 19 |
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