To receive competitive purchasing options on part number 6011T94G02 by General Electric Company, look no further than NSN Direct. For your reference, this item has the NSN 2840-00-134-4969 and is listed with the description “Stator Sector Contr.” If this matches your needs, we encourage you to fill out the partially-completed quote request form on this page to kick off procurement. By providing comprehensive information about your requirements, such as your desired quantity, pricing, and fulfillment speed, our experts can formulate the most fitting solutions for you. We want to ensure that this process is quick and effortless, so we routinely respond to requests within 15 minutes of receiving and reviewing them.
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In addition to our streamlined quotation service, we also aim to make the process of finding products simple. As such, if you require other General Electric Company parts produced under the CAGE Code 99207, you can peruse our manufacturer or CAGE Code catalogs, or use our search engine and filters. Furthermore, if you want to locate items similar to part number 6011T94G02, you can glean from the first four digits of its NSN 2840-00-134-4969 that it belongs to the FSC 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components. This being said, do not hesitate to request quotes on part number 6011T94G02 and any other NSN parts that we feature to experience unrivaled procurement.
NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
2840-00-134-4969 Item PartTypeName: STATOR SECTOR,CONTR | 2840 | 001344969 | 0 | N | ||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
U | U | 0 | ||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
6011T94G02 | 3 | 2 | 3 |
MRC | Criteria | Characteristic |
---|---|---|
FEAT | SPECIAL FEATURES | HARDNESS TO BE ROCKWELL COLLINS 35-48 ON AIRFOILS AND TO BE CHECKED BY SAMPLE VANE PROCESSED ALONG WITH ASSEMBLY THROUGH BRAZING AND HEAT TREAT CYCLE |
SPCL | SPECIAL TEST FEATURES | FLOURESCENT PENETRANT INSPECT PER P3T52 CL-C IMPERFECTIONS AS CRACKS,VOIDS,POROSITY ARE ACCEPTABLE WITHIN THE FOLLOWING LIMITS: (1) NO CRACKS OR FOLDS ALLOWED,(2) NO OTHER IMPERFECTIONS ALLOWED EXCEPT THOSE PERMITTED IN PART SPECIFICATIO |
SUPP | SUPPLEMENTARY FEATURES | SURFACES BETWEEN AIRFOIL SECTIONS MUST BLEND TO FORM A SMOOTH CONTOUR THROUGHOUT THE FULL LENGTH OF THE VANE; RAII AT LEADING AND TRAILING EDGES MUST BLEND SMOOTHLY WITH AIRFOIL CONTOURS |
TEXT | GENERAL CHARACTERISTICS ITEM DESCRIPTION | BRAZE ASSEMBLY: BRAZE AND SOLUTION TREAT AT 1875 DEGREES FAHRENHEIT ( OR-25 DEGREES) FOR 8 HOURS; AGE IN VACUUM OR AIR ATMOSPHERE FURNACE AT 1325F ( OR-25) FOR 8 HOURS; FURNACE COOL TO 1150F ( OR-15) AT 100 F/HOUR; HOLD AT 1150F |
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