Aerospace Performance Parts is pleased to offer immediate purchasing options for United Technologies Corporation part number 4040521, which you have taken interest in. This Plate Component Mounting Aircraf item is listed alongside the NSN 2840-01-298-2646 for ease of identification, with various additional information provided on this page for your reference. Should you wish to obtain solutions on this particular listing, we invite you to complete the Request for Quote (RFQ) form on this page at your earliest convenience. Responses are always offered shortly after we receive and review each request, with solutions we give being fully based on the details we are provided.
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If you happen to require expedited shipping for part number 4040521 or any other FSC 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components components we carry from United Technologies Corporation under CAGE Code 52661, be sure to let us know as soon as possible. We would be happy to discuss the options that we can potentially provide, our track record of on-time delivery being a testament to our dedication to customer satisfaction. You can either include such details within your request, or get in touch with staff directly. Otherwise, request a quote on NSN 2840-01-298-2646 part number 4040521 today, knowing we will support all your operational needs with care.
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 2840-01-298-2646 Item PartTypeName: PLATE,COMPONENT MOUNTING,AIRCRAF | 2840 | 012982646 | 0 | N | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| U | A | |||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| 4040521 | 2 | 2 | 3 |
| MRC | Criteria | Characteristic |
|---|---|---|
| ABHP | OVERALL LENGTH | 2.750 INCHES MINIMUM AND 2.770 INCHES MAXIMUM |
| ABMK | OVERALL WIDTH | 1.365 INCHES MINIMUM AND 1.385 INCHES MAXIMUM |
| ABPX | MATERIAL THICKNESS | 0.065 INCHES MINIMUM AND 0.075 INCHES MAXIMUM |
| AGAV | END ITEM IDENTIFICATION | ACFT ENG F-100-200A |
| CRTL | CRITICALITY CODE JUSTIFICATION | AGAV |
| CZBJ | ENGINE SECTION LOCATION | COMPRESSOR |
| FEAT | SPECIAL FEATURES | WAS PLATE,MOUNTING COMPONENT,TURBINE ENGINE |
| MATT | MATERIAL | TITANIUM ALLOY OVERALL |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | AMS 4911 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
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