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 6011T94G06, a General Electric Company item that is listed alongside the description “Stator Sector Contr” and the NSN 2840001344969. To guarantee a swift procurement process for NSN part number 6011T94G06, 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 6011T94G06 is manufactured by General Electric Company, it is specifically done so under CAGE Code 99207, 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 2840-00-134-4969, 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 |
|---|---|---|---|---|---|---|
| 2840-00-134-4969 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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