Buy Mil Spares is your sourcing solution for top-quality military and defense parts, aerospace parts, and other similar products that are necessary for operational fulfillment. You have reached the RFQ page for part number 1284M82G05, a Shroud Segment Turbine Aircraft item that is listed with the NSN 2840-01-200-6464 for an ease of identification. Manufactured by Moeller Mfg Company Inc and readily available for procurement today, you are always welcome to request a quote on this NSN part to receive tailored pricing information and fulfillment options from our team. Simply offer us important information like your desired quantity, price, and fulfillment timeframe, and our team will supply you with a tailored quote on part number 1284M82G05 in 15 minutes or less.
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To ensure that customers quickly identify and procure exact items, we list everything with as much relevant information as possible. For example, while part number 1284M82G05 is manufactured by Moeller Mfg Company Inc, it is specifically done so under CAGE Code 08244, a unique identifier assigned to a specific facility by the DLA that supplies to various government or defense agencies. Furthermore, using the first digits of the NSN 2840-01-200-6464, one can also determine that this part falls under FSC 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components. With this in mind, continue exploring our website today, and see how we can help you secure competitive pricing and rapid lead times on all desired NSN parts.
NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
2840-01-200-6464 Item PartTypeName: 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 | 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 | 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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