Thank you for your interest in General Electric Company part number 6011T94G02, a Stator Sector Contr item that we offer here on Aerospace Materials Supply. This product is listed with the NSN 2840-00-134-4969, and you can obtain customized procurement solutions on this component from our team members by completing and submitting the form below. For our specialists to best deliver quotes that accommodate your specifications, please be sure we are presented with essential details like your target price, desired quantity, and anticipated fulfillment timeline. Once we have the opportunity to receive and review your submission, we will strive to provide a tailored response for your consideration within 15 minutes or less.
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Besides part number 6011T94G02, you may browse our platform further for similar components produced by General Electric Company under the CAGECode 99207, as well as additional products that are categorized under FSC 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components. If you have any questions regarding our services or the NSN 2840-00-134-4969 items that we sell, you may always give us a call or email, as we would be delighted to assist you in any way that we can. Otherwise, we encourage you to request a quote for part number 6011T94G02 at your earliest convenience.
| 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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