Welcome to our online Request for Quote (RFQ) service, where you can fill out and submit the form provided below to obtain tailored procurement options from our team of industry experts. You have taken interest in part number 17P6W8401-505, which is a Panel Structural Aircraft item from Boeing Company The that is listed with the NSN 1560-01-528-0878 for quick identification. Should you wish to move forward with quotation for this listing, be sure that you supply us with key details like your target pricing, quality, and delivery date. This information is what we will base presented quotes on, with responses offered shortly after the receipt and review of each form.
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To ensure that customers only procure exact items of need, we present our offerings with as much relevant data as possible. For example, part number 17P6W8401-505 was specifically produced by Boeing Company The under the CAGE Code 88277, providing traceability. Furthermore, with the NSN 1560-01-528-0878, one can also determine that this listing falls under Federal Supply Class (FSC) 1560 Airframe Structural Components. Alongside such details, all purchases will come delivered with any applicable qualifying certifications, furthering the reliability of our purchasing options. With this in mind, be sure to request a quote on part number 17P6W8401-505, and we will be in touch.
NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
1560-01-528-0878 Item PartTypeName: PANEL,STRUCTURAL,AIRCRAFT | 1560 | 015280878 | 0 | P | ||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
U | A | 0 | ||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
17P6W8401-505 | 6 | 2 | 3 |
MRC | Criteria | Characteristic |
---|---|---|
MRC | Decoded Requirement | Clear Text Reply |
FEAT | Special Features | M/O CARBON/EPOXY COMPOSITE AND GLASS FIBER/EPOXY COMPOSITE PLYS POLYAMIDE PAPER HONEYCOMB CORE; NHA 17P6W8454; U/O 17A150 THRU 17A999 |
CZEJ | Aircraft Station Number | XRS175.410 TO XRS277.75 |
CZEK | Aircraft Mission Design Series | C-17 |
MDCL | Material Document And Classification | DMS2288 TYPE 2 CLASS 2 GRADE 0 MFR REF 1ST MATERIAL RESPONSE AND DMS2288 TYPE 3 CLASS 2 GRADE D MFR REF 2ND MATERIAL RESPONSE AND DMS 1974 TYPE 3 CLASS 2 GRADE 3 MFR REF 3RD MATERIAL RESPONSE |
AARN | Fabrication Method | COMPOSITE |
CZDJ | Aircraft Location | PANEL-UPPER NO.1, WING FIXED TRAILING EDGE |
MATT | Material | PLASTIC EPOXY AND GLASS FIBER AND PLASTIC POLYAMIDE |
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