Thank you for taking an interest in the various military and defense parts, aerospace parts, and other items that we offer. You have reached the RFQ page for part number 540-011-020-7, a Bell Helicopter Textron Inc item with the NSN 1615004956590 that is listed alongside the description “Retainer Weight Blade.” If you are interested in part number 540-011-020-7 and wish to learn more about your purchasing options, be sure to submit the form below at your earliest convenience while supplying us with important information concerning your needs and restrictions alike. Once we have a chance to receive and review your completed form, a member of our staff will reach out to you in 15 minutes or less to present a tailored solution for your comparisons.
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To ensure that shopping with us is as simple as possible, we make it easy to identify and procure exact items by listing parts alongside all applicable designations and information. For example, part number 540-011-020-7 is specifically listed with the NSN 1615-00-495-6590, and this code can be used to determine that it falls under FSC 1615 Helicopter Rotor Blades Drive Mechanisms and Components. Additionally, while tracing back to Bell Helicopter Textron Inc, this NSN part was specifically produced under CAGE Code 97499. With our services and dedication to simple procurement in mind, get started with us today!
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 1615-00-495-6590 Item PartTypeName: RETAINER,WEIGHT,BLADE | 1615 | 004956590 | 0 | N | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| 7 | U | |||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| 540-011-020-7 | 5 | 2 | 3 |
| MRC | Criteria | Characteristic |
|---|---|---|
| TEXT | GENERAL CHARACTERISTICS ITEM DESCRIPTION | ALUMINUM ALLOY,QQ-A-250/4 TEMPER T3,DIM.,2.400 IN. NOM LG,1.440 IN. NOMW AT BOTTOM,1.600 IN. NOM W AT 0.700 IN. FROM BOTTOM,1.360 IN. NOM W AT1.042 IN. FROM TOP,0.580 IN. NOM W AT TOP,0.160 IN. NOM MATERIAL THICKNESSTWO HOLES 0.315 IN. MIN |
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