Thank you for taking interest in United Technologies Corporation part number 4014758, which is listed with the NSN 2840-01-324-1163 and a product description of “Plate Component Mounting Aircraf.” In order to receive procurement options on this particular listing, we ask that you fill out and submit the form provided below with as much information as you can concerning your needs. By supplying our staff with key details on your desired quantity, pricing target, and expedited fulfillment timeframe, we can respond with a quote that has been specifically tailored to your unique specifications. We also ask that you make us aware of any restrictions that you may have as soon as possible, such as if you have a time constraint or are seeking unlisted items.
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Alongside part number 4014758, you are encouraged to continue exploring our collection curated catalogs to find additional items that can accompany this Plate Component Mounting Aircraf part with the NSN 2840-01-324-1163. For example, you can browse other United Technologies Corporation components that were produced under CAGE Code 77445 or listings that belong to FSC 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components with ease on our website, with search tools provided for quick location. Furthermore, our staff is just a call or email away from assisting you with any inquiries or requests, so be sure to get started on the quotation process for part number 4014758 and other desired offerings on Aerospace Spare.
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 2840-01-324-1163 Item PartTypeName: PLATE,COMPONENT MOUNTING,AIRCRAF | 2840 | 013241163 | 0 | N | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| U | A | 0 | ||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| 4014758 | 5 | 2 | 3 |
| MRC | Criteria | Characteristic |
|---|---|---|
| ABMZ | DIAMETER | 7.650 INCHES MINIMUM AND 7.680 INCHES MAXIMUM |
| ABPX | MATERIAL THICKNESS | 0.040 INCHES NOMINAL |
| CZBJ | ENGINE SECTION LOCATION | TURBINE |
| AGAV | END ITEM IDENTIFICATION | AIRCRAFT ENGINE F100-PW-100/200/220 |
| CQFM | HARDNESS RATING | 30.0 ROCKWELL C MINIMUM OUTER CASE AND 38.0 ROCKWELL C MAXIMUM OUTER CASE |
| CRTL | CRITICALITY CODE JUSTIFICATION | AGAV |
| MATT | MATERIAL | STEEL OUTER CASE |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | AMS5504 ASSN STD 1ST MATERIAL RESPONSE OUTER CASE AND AMS5613 ASSN STD 2ND MATERIAL RESPONSE OUTER CASE |
| ABHP | OVERALL LENGTH | 0.038 INCHES MINIMUM AND 0.043 INCHES MAXIMUM |
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