Request a Quote on 37D401131P101 Kerns Manufacturing Corp Part with the NSN 2840007238221
Thank you for taking an interest in part number 37D401131P101, a Kerns Manufacturing Corp product we have in stock that is listed alongside the NSN 2840007238221 and the description “Cover Sump Front Frame.” As part number 37D401131P101 is readily available for purchase on our website at any time, you are invited to fill out and submit the RFQ form provided on this page for the means of requesting a quote for your comparisons. All that we ask is that you supply us with important information such as your target price and expected shipping time frame so that we can best tailor a solution that caters to your unique needs and restrictions alike.
To ensure that you only procure the exact items you require for carrying out operations, we list all aerospace parts, military and defense parts, and other product offerings with all applicable information for identification. For example, part number 37D401131P101 is listed alongside the NSN 2840007238221, meaning that it also belongs to FSC . Furthermore, this NSN part is specifically manufactured under CAGE Code , a unique identifier belonging to the manufacturer for a specific facility. With all of this in mind, kick off purchasing with us today and see why so many customers steadily choose us for their operational needs.
| Part Number | 37D401131P101 |
| Description | Cover Sump Front Frame |
| Manufacturer | Aerospace Industries |
| NSN | 2840-00-723-8221(2840007238221) |
| Item Name | Cover Sump Front Frame |
| CAGE Code | 0AMR1 |
| NIIN | 00-723-8221(007238221) |
| FSC Code | 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components |
| FSG Code | 28 Engines, Turbines, and Components |
| INC Code | 77777 |
| NCB Code | 00 |
| Country | USA |
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NSN Information for Part Number 37D401131P101 with NSN 2840-00-723-8221, 2840007238221
Characteristics Data of NSN 2840-00-723-8221, 2840007238221
| MRC | Criteria | Characteristic |
|---|---|---|
| AGAV | END ITEM IDENTIFICATION | J-85 AIRCRAFT ENGINE |
| TEXT | GENERAL CHARACTERISTICS ITEM DESCRIPTION | FINISH ANODIZE,3 HOLES EQUALLY SPACED 0.161 IN. DIA,0.050 IN. THICKNESSOF MATERIAL |
