Part No. : 5HW84784-108 | Alternate P/N : 5HW84784108 | Manufacturer : the boeing company |
Item Name: panel structural aircraft | NSN: 1560-01-518-6304 (1560015186304) | CAGE Code: 81205 |
FSC: 1560 Airframe Structural Components |
If you require part number 5HW84784-108 from The Boeing Company which is described as a Panel Structural Aircraft component ASAP Logistic Solutions is your sourcing solution. On this page, you can request a quote on part number 5HW84784-108 which is listed under the Federal Supply Class 1560 Airframe Structural Components. To ensure that you only procure the exact item you need to be sure to note that this particular product is listed with the NSN 1560015186304 and was produced under the CAGE Code 81205. To learn more about this listing or to simply initiate the purchasing process, complete and submit the RFQ form on this page for part 5HW84784-108 today Within 15 minutes of receiving and reviewing a completed request based on the information you provide a member of our staff will contact you to provide a tailored solution to your comparison needs.
NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
1560-01-518-6304 Item PartTypeName: PANEL,STRUCTURAL,AIRCRAFT | 1560 | 015186304 | 0 | P | ||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
7 | A | 0 | ||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
5HW84784-108 | 6 | 2 | 3 |
MRC | Criteria | Characteristic |
---|---|---|
AGAV | END ITEM IDENTIFICATION | F-22 RAPTOR |
CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | INSERT |
CZDJ | AIRCRAFT LOCATION | UPPER FLAPERON |
CZEK | AIRCRAFT MISSION DESIGN SERIES | F-22A |
FEAT | SPECIAL FEATURES | WIND SWEPT SURFACE CRITICAL ITEM; OPPOSITE -107; M/O: CARBON/BMI COMPOSITE MATERIAL |
AGAV | END ITEM IDENTIFICATION | F-22 RAPTOR |
CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | INSERT |
CZDJ | AIRCRAFT LOCATION | UPPER FLAPERON |
CZEK | AIRCRAFT MISSION DESIGN SERIES | F-22A |
FEAT | SPECIAL FEATURES | WIND SWEPT SURFACE CRITICAL ITEM; OPPOSITE -107; M/O: CARBON/BMI COMPOSITE MATERIAL |
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