Thank you for choosing to partner with National Stock Number Shop for the Shroud Segment Turbine Aircraft NSN parts you require. On this page, you can submit a quote request for United Technologies Corporation part number 473497, a component that can also be found by inputting NSN 2840009944730 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 77445 to uniquely identify items in a standardized manner. Additionally, we utilize Federal Supply Classes (FSCs) to organize our stock, ensuring customers can find United Technologies Corporation 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 2840009944730 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 |
|---|---|---|---|---|---|---|
| 2840-00-994-4730 Item PartTypeName: SHROUD SEGMENT,TURBINE,AIRCRAFT | 2840 | 009944730 | 0 | N | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| U | A | |||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| 473497 | 1 | 9 | 5 |
| MRC | Criteria | Characteristic |
|---|---|---|
| ABHP | OVERALL LENGTH | 1.435 INCHES MINIMUM AND 1.455 INCHES MAXIMUM |
| CRTL | CRITICALITY CODE JUSTIFICATION | FEAT |
| CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | SHROUD TURBINE STATOR,3 STAGE,ASSY OF |
| CZBJ | ENGINE SECTION LOCATION | TURBINE |
| CZCJ | STAGE NUMBER | 3 |
| FEAT | SPECIAL FEATURES | USED ON THE PW103 ENGINE ONLY |
| MATT | MATERIAL | ALUMINUM ALLOY OVERALL |
| RDAL | REFERENCE DATA AND LITERATURE | T.O. 2J-TF33-4 FIG 32,IND 21 |
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