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 9686M32G11, a General Electric Company item that is listed alongside the description “Frame Rear Aircraft Gas Turbine” and the NSN 2840004934651. To guarantee a swift procurement process for NSN part number 9686M32G11, 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 9686M32G11 is manufactured by General Electric Company, it is specifically done so under CAGE Code 07482, 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 2840-00-493-4651, 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 |
---|---|---|---|---|---|---|
2840-00-493-4651 Item PartTypeName: FRAME,REAR,AIRCRAFT GAS TURBINE | 2840 | 004934651 | 0 | N | ||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
7 | A | |||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
9686M32G11 | 6 | 2 | 3 |
MRC | Criteria | Characteristic |
---|---|---|
AGAV | END ITEM IDENTIFICATION | GENERAL ELECTRIC MODEL TF39 ENGINE |
CRTL | CRITICALITY CODE JUSTIFICATION | FEAT |
CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | ORIGINAL NAME FRAME,TURBINE |
CZLB | NUMBER OF VARIABLE GUIDE VANES | 8 |
FEAT | SPECIAL FEATURES | USED ON THE LOW PRESSURE TURBINE FRAME ONLY; REPL BY P/N 9686M32G13 AND 9686M32G14 |
RDAL | REFERENCE DATA AND LITERATURE | T.O. 2J-TF39-4,FIG 183,IND 17 |
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