| Mfg Part Number: 1284M82G05 | NSN : 2840-01-200-6464 | NIIN : 012006464 |
| CAGE Code : 28884 | Manufacturer: Tss Technologies Inc | Item Name : Shroud Segment Turbine Aircraft |
| FSC : 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components | Description: Shroud Segment Turbine Aircraft |
If you are in the market for Shroud Segment Turbine Aircraft items, such as nsn part number 1284M82G05, then look no further than Integrated Jet Parts! We currently have this Tss Technologies Inc item in stock and it is listed under the NSN 2840-01-200-6464, allowing you to locate it quickly and easily. As such, we invite you to fill out an RFQ form for this component to receive a customized quote within 15 minutes or less. For ease of item identification, nsn part number 1284M82G05 with the specific NSN 2840-01-200-6464 can also be found alongside CAGE Code 28884; however, we carry an array of other NSN products, all of which have been sourced from trusted manufacturers like Tss Technologies Inc.
At Integrated Jet Parts, we operate with AS9120B, ISO 9001:2015, and FAA AC 00-56B accreditation, alongside a strict NO CHINA SOURCING pledge to ensure that customers can always rely on the caliber of our offerings. Initiate the purchasing process for nsn part number 1284M82G05 from Tss Technologies Inc today and see how Integrated Jet Parts can serve as your strategic sourcing partner. For additional inquiries, call or email us directly; we are on standby 24/7x365!
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 2840-01-200-6464 Item Description: Shroud Segment Turbine Aircraft | 2840 | 012006464 | 0 | N | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| U | A | 0 | ||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| 1284m82g05 | 6 | 2 | 5 |
| 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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