Thank you for your interest in Tei Tusas Motor San A S part number 1276M30G02, a Case Turbine Aircraft Gas Turbin item that we offer here on Aerospace Materials Supply. This product is listed with the NSN 2840-01-447-2846, 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 1276M30G02, you may browse our platform further for similar components produced by Tei Tusas Motor San A S under the CAGECode T0545, 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 2840-01-447-2846 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 1276M30G02 at your earliest convenience.
NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
2840-01-447-2846 Item PartTypeName: CASE,TURBINE,AIRCRAFT GAS TURBIN | 2840 | 014472846 | 0 | N | ||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
7 | A | 0 | ||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
1276M30G02 | 3 | 1 | 8 |
MRC | Criteria | Characteristic |
---|---|---|
ABHP | OVERALL LENGTH | 2.359 INCHES MINIMUM AND 2.383 INCHES MAXIMUM |
AGAV | END ITEM IDENTIFICATION | ACFT ENG F110GE129 |
APGF | DESIGN TYPE | AXIAL COMPRESSOR |
CRTL | CRITICALITY CODE JUSTIFICATION | ABHP AND CZBJ AND FEAT |
CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | COVER,COOLING AIR-HIGH PRESSURE TURBINE NOZZLE,OUTER |
CZBJ | ENGINE SECTION LOCATION | HIGH PRESSURE TURBINE |
FEAT | SPECIAL FEATURES | USED ON THE NOZZLE ASSEMBLY AND SEGMENTS, SEALS AND SUPPORTS |
RDAL | REFERENCE DATA AND LITERATURE | T.O. 2J-F110-14, FIG 74, IND 17 |
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