Aerospace Engineering Solutions is proud to offer immediate purchasing options on General Electric Company part number 6011T94G06, a Stator Sector Contr product we carry that is listed with the NSN 2840-00-134-4969 for ease of identification. If you would like to learn more about this item, be sure to complete the Request for Quote (RFQ) form provided on this page. By including essential details like your target price, desired quantity, and expected fulfillment timeline, you are ensured a fully customized quote from our team.
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For your reference, this product is traceable to General Electric Company through the CAGE Code 99207, as well as categorized under FSC 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components based on the first four digits of the NSN 2840-00-134-4969. Using such information, you can easily narrow down exact items of need for an ease of procurement. With our quotation service in mind, be sure to submit a completed form when you are ready to begin. Should you wish to speak with one of our representatives to discuss services, you can also give us a call or email at your convenience. With all that we offer, choose Aerospace Engineering Solutions for part number 6011T94G06 and other NSN items of need.
| 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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