| Mfg Part Number: 68A230001-2005 | Alternate P/N: 68A2300012005 | NSN : 1560-01-481-8354 |
| NIIN : 014818354 | CAGE Code : 76301 | Manufacturer: The Boeing Company |
| Item Name : Plate Structural Aircraft | FSC : 1560 Airframe Structural Components |
Thank you for your continued interest in the parts associated with the NSN 1560-01-481-8354, those of which are readily available for purchase on Automatize Electronics. The Plate Structural Aircraft item associated with the part number 68A230001-2005, by The Boeing Company, is currently available on our database; thus, if you wish to begin the part number 68A230001-2005 procurement process, we ask that you please fill out and submit an Instant RFQ form detailing your requirements on parts needed. This includes desired quantities, target prices, expected shipping time frames, and more, as applicable. Upon receival, our representatives will harness your provided information and formulate a solution which satisfies your operational needs in just 15 minutes or less.
With our global supply chain stretching across the United States, Canada, and the United Kingdom, Automatize Electronics can provide expedited shipping on select NSN products with the CAGE Code 76301, strategically assisting entities facing an Aircraft on Ground (AOG) situation or other unique time constraint. Operating with a strict NO CHINA SOURCING pledge, all items are shipped alongside their manufacturer trace documentation or qualifying certifications, ensuring that customers feel confident in every purchase made. With cost savings and rapid lead times bolstering every order, experience all of what Automatize Electronics has to offer on products with the NSN 1560-01-481-8354 by submitting your RFQ for parts by The Boeing Company. submit a quote for the part number 68A230001-2005, today!
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 1560-01-481-8354 Item Description: Plate Structural Aircraft | 1560 | 014818354 | 0 | P | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| 7 | A | 0 | ||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| 68a230001-2005 | 6 | 2 | 3 |
| MRC | Criteria | Characteristic |
|---|---|---|
| ABPX | Material Thickness | 0.048 INCHES NOMINAL |
| MDCL | Material Document And Classification | MIL-S-22499 CLASS 2 TYPE 1 MIL SPEC SINGLE MATERIAL RESPONSE |
| CZEK | Aircraft Mission Design Series | F-15 |
| ABMK | Overall Width | 0.750 INCHES NOMINAL |
| CZDJ | Aircraft Location | VERTICAL STABILIZER |
| FEAT | Special Features | NHA 68A230021; U/O F-15C CUM270 AND UP, F-15D CUM45 AND UP, F-15E CUM1-128; INCLUDES 31 0.218 IN. DIA. HOLES ALONG LGTH |
| CXCY | Part Name Assigned By Controlling Agency | SHIM |
| MRC | Decoded Requirement | Clear Text Reply |
| MATT | Material | ALUMINUM ALLOY 5052 |
| ABHP | Overall Length | 40.450 INCHES NOMINAL |
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