To receive competitive purchasing options on part number 5HW82821-135 by The Boeing Company, look no further than NSN Direct. For your reference, this item has the NSN 1560-01-487-5296 and is listed with the description “Panel Structural 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 The Boeing Company parts produced under the CAGE Code 81205, 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 5HW82821-135, you can glean from the first four digits of its NSN 1560-01-487-5296 that it belongs to the FSC 1560 Airframe Structural Components. This being said, do not hesitate to request quotes on part number 5HW82821-135 and any other NSN parts that we feature to experience unrivaled procurement.
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 1560-01-487-5296 Item PartTypeName: PANEL,STRUCTURAL,AIRCRAFT | 1560 | 014875296 | 0 | P | A | |
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| 7 | A | A | 0 | |||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| 5HW82821-135 | 6 | 2 | 3 |
| MRC | Criteria | Characteristic |
|---|---|---|
| FEAT | Special Features | WIND SWEPT SURFACE CRITICAL ITEM; OPPOSITE -136; C/O: 5HW82822-147 ACCESS PANEL, STUD BOLT (4); DIM. ARE STOCK MATERIAL; M/O 6AL-4V (AD-1) ANN TITANIUM PLATE |
| ABMK | Overall Width | 6.000 INCHES NOMINAL |
| AGAV | End Item Identification | F-22 RAPTOR |
| CZEK | Aircraft Mission Design Series | F-22A |
| ABHP | Overall Length | 11.000 INCHES NOMINAL |
| MRC | Decoded Requirement | Clear Text Reply |
| CZDJ | Aircraft Location | PANEL ASSEMBLY - ACCESS, RIB 4 AND 6 |
| MDCL | Material Document And Classification | AMS-T-9046 ASSN STD SINGLE MATERIAL RESPONSE |
| MATT | Material | TITANIUM |
| CXCY | Part Name Assigned By Controlling Agency | PANEL ASSEMBLY, AFT |
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