Thank you for taking an interest in part number 214-040-845-103, a Bell Helicopter Textron Inc product we have in stock that is listed alongside the NSN 2995012567641 and the description “Oil Pump Assembly Engine.” As part number 214-040-845-103 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.
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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 214-040-845-103 is listed alongside the NSN 2995-01-256-7641, meaning that it also belongs to FSC 2995 Miscellaneous Engine Accessories Aircraft. Furthermore, this NSN part is specifically manufactured under CAGE Code 97499, 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.
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 2995-01-256-7641 Item PartTypeName: OIL PUMP ASSEMBLY,ENGINE | 2995 | 012567641 | 0 | N | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| U | A | 0 | ||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| 214-040-845-103 | 6 | 3 | 1 |
| MRC | Criteria | Characteristic |
|---|---|---|
| AGAV | END ITEM IDENTIFICATION | AH-1W ACFT |
| FEAT | SPECIAL FEATURES | 5.870 IN.O/A L;SPEED 6925 RPM;FLOW 16.25-18-10 GPM AT 180 DEG F AND 150 PSIG;DISCHARGE PRESSURE 160 PLUS OR MINUS 10 PSID AT 180 DEG FAHRENHEIT;OIL PLUS MIL-L-7808 OR MIL-L-23699 |
| ZZZY | REFERENCE NUMBER DIFFERENTIATING CHARACTERISTICS | AS DIFFERENTIATED BY THE SOURCE CONTROL DWG NO. |
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