Thank you for taking an interest in the various military and defense parts, aerospace parts, and other items that we offer. You have reached the RFQ page for part number 6809081, a Rolls Royce Corporation item with the NSN 2840008770065 that is listed alongside the description “Blade Compressor Aircraft Gas Tu.” If you are interested in part number 6809081 and wish to learn more about your purchasing options, be sure to submit the form below at your earliest convenience while supplying us with important information concerning your needs and restrictions alike. Once we have a chance to receive and review your completed form, a member of our staff will reach out to you in 15 minutes or less to present a tailored solution for your comparisons.
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To ensure that shopping with us is as simple as possible, we make it easy to identify and procure exact items by listing parts alongside all applicable designations and information. For example, part number 6809081 is specifically listed with the NSN 2840-00-877-0065, and this code can be used to determine that it falls under FSC 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components. Additionally, while tracing back to Rolls Royce Corporation, this NSN part was specifically produced under CAGE Code 63005. With our services and dedication to simple procurement in mind, get started with us today!
| 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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