Thank you for your interest in Mtu Aero Engines Gmbh part number 777886CL7, a Lock Ring Turbine Nozzle Aircraf item that we offer here on Aerospace Materials Supply. This product is listed with the NSN 2840-01-124-0725, 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 777886CL7, you may browse our platform further for similar components produced by Mtu Aero Engines Gmbh under the CAGECode 50381, 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 2840-01-124-0725 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 777886CL7 at your earliest convenience.
NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
2840-01-124-0725 Item PartTypeName: LOCK RING,TURBINE NOZZLE,AIRCRAF | 2840 | 011240725 | 0 | N | ||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
U | A | |||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
777886CL7 | 6 | 9 | 5 |
MRC | Criteria | Characteristic |
---|---|---|
ABKV | OUTSIDE DIAMETER | 34.878 INCHES MINIMUM AND 34.908 INCHES MAXIMUM |
ADUM | OVERALL THICKNESS | 0.143 INCHES MINIMUM AND 0.147 INCHES MAXIMUM |
AGAV | END ITEM IDENTIFICATION | ACFT ENG TF33 |
CRTL | CRITICALITY CODE JUSTIFICATION | AGAV |
CZCJ | STAGE NUMBER | 3 |
FEAT | SPECIAL FEATURES | MATL AMS 5731 |
MATT | MATERIAL | STEEL |
RDAL | REFERENCE DATA AND LITERATURE | 2J-TF33-34,FIGURE 28,INDEX 21 |
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