To receive competitive purchasing options on part number L2100204-015 by Boeing Company The, look no further than NSN Direct. For your reference, this item has the NSN 1560-01-506-8630 and is listed with the description “Tip Aircraft.” If this matches your needs, we encourage you to fill out the partially-completed quote request form on this page to kick off procurement. By providing comprehensive information about your requirements, such as your desired quantity, pricing, and fulfillment speed, our experts can formulate the most fitting solutions for you. We want to ensure that this process is quick and effortless, so we routinely respond to requests within 15 minutes of receiving and reviewing them.
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In addition to our streamlined quotation service, we also aim to make the process of finding products simple. As such, if you require other Boeing Company The parts produced under the CAGE Code 43999, you can peruse our manufacturer or CAGE Code catalogs, or use our search engine and filters. Furthermore, if you want to locate items similar to part number L2100204-015, you can glean from the first four digits of its NSN 1560-01-506-8630 that it belongs to the FSC 1560 Airframe Structural Components. This being said, do not hesitate to request quotes on part number L2100204-015 and any other NSN parts that we feature to experience unrivaled procurement.
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 1560-01-506-8630 Item PartTypeName: TIP,AIRCRAFT | 1560 | 015068630 | 0 | P | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| 7 | A | 0 | ||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| L2100204-015 | 6 | 2 | 3 |
| MRC | Criteria | Characteristic |
|---|---|---|
| ABMK | OVERALL WIDTH | 2.000 INCHES NOMINAL |
| CRTL | CRITICALITY CODE JUSTIFICATION | FEAT |
| CZDJ | AIRCRAFT LOCATION | TIP, HORIZONTAL STABILIZER |
| FEAT | SPECIAL FEATURES | U/0 B-1B; DIMS ARE STOCK MATERIAL; MATERIAL IS AL CLAD SHEET, HEAT TREATR TO T-62 PER ST0111LA0009, FINISH 09 PRIOR TO BONDING |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/5, T-62 FED SPEC SINGLE MATERIAL RESPONSE |
| ABHP | OVERALL LENGTH | 84.000 INCHES NOMINAL |
| ABPX | MATERIAL THICKNESS | 0.020 INCHES NOMINAL |
| CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | LEADING EDGE FACE SHEET |
| CZEK | AIRCRAFT MISSION DESIGN SERIES | B-1B |
| MATT | MATERIAL | ALUMINUM ALLOY 2024 |
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