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 your continued interest in the various parts and components currently available on The NSN Mart. Here, our customers will find our NSN RFQ Page for Shroud Segment Turb parts with the NSN 2840-01-200-6464, among others from the manufacturer Tss Technologies Inc. For particular equipment such as part number 1284M82G05, the submission of a completed RFQ form will provide customers with a quote on any desired part in just 15 minutes or less. Upon receival, our expert market representatives will use your offered information to construct a quote paramount to your operations with rapid turnaround times and cost savings at our forefront.
As our robust supply chain stretches across the United States, we are able to supply entities facing Aircraft on Ground (AOG) delays, or other unique time constraints, with expedited shipping on select NSN 2840-01-200-6464 items for immediate procurement. Operating as an AS9120B, ISO 9001:2015, and FAA AC 00-56B accredited enterprise, products listed on our database are upheld to rigorous quality assurance testing, inspection, and cross-referencing before shipment. Functioning as the only independent distributor with a NO CHINA SOURCING pledge, you can depend on The NSN Mart for authentic items like those listed alongside the CAGE Code 28884 by Tss Technologies Inc.
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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