You have arrived on the Request for Quote (RFQ) page for part number 6809081, a Rolls Royce Corporation component that is listed with the product description “Blade Compressor Aircraft Gas Tu” and NSN 2840-00-877-0065 for fast identification. By using the form supplied below, you can offer details regarding your requirements to secure customized procurement solutions for your consideration. As our goal is to provide quick service, you can expect a response within 15 minutes of our staff members reviewing your submission. Alternatively, if you use the email or phone number at the bottom of the webpage, you can directly connect with our experts to discuss your needs.
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Alongside Rolls Royce Corporation part number 6809081, you can seamlessly search for more items from this manufacturer or CAGECode 63005 using our curated catalogs. Similarly, we also offer means for locating other products that belong to FSC 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components, which this component falls under having the NSN 2840-00-877-0065. Whether you desire part number 6809081 or other NSN components, you can rest assured that our entire inventory is sourced from reputable manufacturers and suppliers. Bearing this in mind, kick off procurement today to see why so many customers select Aero Defence Solutions as their trusted purchasing hub.
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 2840-00-877-0065 Item PartTypeName: BLADE,COMPRESSOR,AIRCRAFT GAS TU | 2840 | 008770065 | 0 | N | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| U | A | 0 | ||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| 6809081 | 2 | 2 | 3 |
| MRC | Criteria | Characteristic |
|---|---|---|
| ABHP | OVERALL LENGTH | 3.753 INCHES NOMINAL |
| AGAV | END ITEM IDENTIFICATION | T56 AIRCRAFT ENGINE |
| CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | BLADE,COMPRESSOR-1ST STAGE |
| MATT | MATERIAL | STEEL CORROSION RESISTING OVERALL |
| ABMK | OVERALL WIDTH | 1.197 INCHES NOMINAL |
| CRTL | CRITICALITY CODE JUSTIFICATION | AGAV |
| FEAT | SPECIAL FEATURES | CONTOUR OF CONCAVE AND CONVEX SIDES OF AIRFOIL SECTIONS MAY VARY WITHIN A .006 BAND PARALLEL TO BASIC; TOLERANCE BAND APPLIES TO SECTION CONTOURS UP TO TANGENT POINT OF LEADING AND TRAILING EDGE RADII; AIRFOIL SURFACES SHALL BLEND SMOOTHLY |
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