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 17P2A6520-3, which is a Panel Structural Aircraft item from Boeing Company The that is listed with the NSN 1560-01-478-1411 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 17P2A6520-3 was specifically produced by Boeing Company The under the CAGE Code 88277, providing traceability. Furthermore, with the NSN 1560-01-478-1411, 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 17P2A6520-3, and we will be in touch.
NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
1560-01-478-1411 Item PartTypeName: PANEL,STRUCTURAL,AIRCRAFT | 1560 | 014781411 | 0 | P | A | |
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
U | A | A | 0 | |||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
17P2A6520-3 | 6 | 2 | 3 |
MRC | Criteria | Characteristic |
---|---|---|
CZDJ | AIRCRAFT LOCATION | WG TO FUS PANEL INSTL, FILLET-UPR, AFT |
SR-5 | MANUFACTURERS CODE | 88277 |
SR-5 | DESIGN CONTROL REFERENCE | 17P2A6520-3 |
FEAT | SPECIAL FEATURES | CONSISTS OF 1(-5) PANEL, 5 RETAINTERS, 8 SEALS AND 81 RIVETS. PANEL MATERIAL IS GLASS FIBER WOVEN FABRIC AND CARBON FIBER WOVEN FABRIC. CORE MATERIAL IS HONEYCOMB POLYMIDE PAPER, OVEREXPANDED |
CZEK | AIRCRAFT MISSION DESIGN SERIES | C-17 |
MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | DMS2288 MFR REF 1ST MATERIAL RESPONSE AND DMS1974 MFR REF 2ND MATERIAL RESPONSE |
SR-5 | THE MANUFACTURERS DATA | |
MATT | MATERIAL | PLASTIC EPOXY AND PLASTIC POLYIMIDE |
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