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Quality guaranteed We sell only warrantied and traceable partsIf you have been searching for 1284M82G05 of Shroud Segment Turb components with NSN 2840012006464 under FSC 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components, look no further than Limitless Aerospace. 1284M82G05 part is listed alongside the other Shroud Segment Turb parts, and it has been manufactured by Tss Technologies Inc (CAGE Code 28884). With current availability through our website, we invite you to request a quick and competitive quote for 1284M82G05 by filling out and submitting the RFQ form below. By providing us with information such as your target price and when you need your parts by, we can ensure that we offer a personalized solution that accommodates your individual needs and requirements.
NSN parts are those that follow the NSN system as dictated by the NATO Standardization Agreements, and they contain a 13-digit serial number to optimize the procurement, stocking, and issuing of items through the federal supply system. On Limitless Aerospace, we make finding the NSN parts and components you need easy, and customers may peruse our robust NSN part catalogues or use our search engine to find specific items with ease. As the only independent distributor with a no China sourcing pledge, we choose to only stock items from top global manufacturers such as Tss Technologies Inc. Get started on the purchasing process for 1284M82G05 today and see how we can serve as your strategic sourcing partner for all of your operational needs.
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 2840-01-200-6464 Item Description: Shroud Segment Turb | 2840 | 012006464 | 0 | N | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| U | A | 0 | ||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| 1284m82g05 | 6 | 2 | 3 |
| MRC | Criteria | Characteristic |
|---|---|---|
| ABHP | OVERALL LENGTH | 12.233 INCHES NOMINAL |
| ABMK | OVERALL WIDTH | 1.890 INCHES NOMINAL |
| AGAV | END ITEM IDENTIFICATION | F110 ACFT ENGINE |
| CRTL | CRITICALITY CODE JUSTIFICATION | AGAV |
| CZBJ | ENGINE SECTION LOCATION | COMPRESSOR |
| CZCJ | STAGE NUMBER | 2 |
| FEAT | SPECIAL FEATURES | OUTER RADIUS 2ND END 11.908 IN.; INNER RADIUS 1ST END 11.393 IN.; INNER RADIUS 2ND END 11.14 IN.; FORMED SHAPE 45 DEG. 57 MIN. 27 SEC.; 11 HOLES 0.3535 IN. DIA. COUNTERBORE 0.520 IN. DIA. W/2 CUTTER RUN OUTS PER EA HOLE |
| MATT | III MATERIAL | ALUMINUM ALLOY 2618 OVERALL |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | AMS4132 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| SFTT | SURFACE TREATMENT | ANODIZE OVERALL |
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