Mfg Part Number: 1284M82G05 | NSN : 2840-01-200-6464 | NIIN : 012006464 |
CAGE Code : 28884 | Manufacturer: Tss Technologies Inc | Item Name : Shroud Segment Turb |
FSC : 2840 Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components |
Thank you for choosing Aircraft Parts Supplier for all your operational needs. You have reached our NSN RFQ Page which features our in-demand NSN 2840-01-200-6464 parts and components such as Shroud Segment Turb manufactured by Tss Technologies Inc. Some of these items include part number 1284M82G05, and various others, all of which have been subjected to a number of quality assurance measures, tests, verifications, and assessments. At Aircraft Parts Supplier, we make it our priority to only source from top global manufacturers that we trust, assuaging the worry of not receiving quality items from us.
The part 1284M82G05 with NSN 2840-01-200-6464 that we feature by the manufacturer Tss Technologies Inc are paired alongside CAGE Code 28884 is available and readt to ship. Aircraft Parts Supplier carries a variety of NSN products, allowing us to be the go-to supplier for countless businesses. If you are familiar with the NSN associated with the item you are in search of, we invite you to take advantage of it. Similarly, other information regarding the NSN items you wish to purchase is equally as helpful, so please provide such details in the provided RFQ form below. When you fill out a form, in return, you will be provided a competitive quote for your comparisons in just 15 minutes or less.
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 | 1 | 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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