Thank you for choosing to partner with National Stock Number Shop for the Damper Turbine Blade Aircraft Tu NSN parts you require. On this page, you can submit a quote request for General Electric Company part number 1807M27, a component that can also be found by inputting NSN 2840014446529 in our search engine. Apart from this item, we also have an array of other in-demand part numbers, all of which can be traced back to a conglomerate of well-known manufacturers that we trust. Explore our expansive part catalogs by scrolling over to our menu and locate products according to manufacturer, NIIN, NSN, and more.
National Stock Number Shop works with numerous government and defense agencies, so we use CAGE Codes like 07482 to uniquely identify items in a standardized manner. Additionally, we utilize Federal Supply Classes (FSCs) to organize our stock, ensuring customers can find General Electric Company parts under the FSC 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components with ease. With this in mind, we encourage you to complete the RFQ form below for NSN 2840014446529 or any others, and see how we can provide you with a customized sourcing solution. For one-on-one assistance, contact us via phone or email at any time; we are available around the clock for customer inquiries!
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| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 2840-01-444-6529 Item PartTypeName: DAMPER,TURBINE BLADE,AIRCRAFT TU | 2840 | 014446529 | 0 | N | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| 7 | A | 0 | ||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| 1807M27 | 5 | 9 | D |
| MRC | Criteria | Characteristic |
|---|---|---|
| APGF | Design Type | AXIAL COMPRESSOR |
| FEAT | Special Features | ORIGNAL NAME DAMPER ASSEMBLY,HIGH PRESSURE TURBINE ROTOR-STAGE 1. G03 ADDED TO PART NUMBER PER CID 219639. THIS ITEM IS PART OF THE HT90 MOD FOR THE TF39 ENGING |
| MRC | Decoded Requirement | Clear Text Reply |
| AGAV | End Item Identification | ACFT ENG TF39 |
| CZBJ | Engine Section Location | HIGH PRESSURE TURBINE |
| CRTL | Criticality Code Justification | AGAV |
| CZCJ | Stage Number | 1 |
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