Thank you for your interest in General Motors Corp part number 6809081, a Blade Compressor Aircraft Gas Tu item that we offer here on Aerospace Materials Supply. This product is listed with the NSN 2840-00-877-0065, 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 6809081, you may browse our platform further for similar components produced by General Motors Corp under the CAGECode 24617, 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 2840-00-877-0065 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 6809081 at your earliest convenience.
| 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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