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 17P2A5204-2, which is a Panel Structural Aircraft item from Boeing Company The that is listed with the NSN 1560-01-518-9434 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 17P2A5204-2 was specifically produced by Boeing Company The under the CAGE Code 88277, providing traceability. Furthermore, with the NSN 1560-01-518-9434, 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 17P2A5204-2, and we will be in touch.
NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
1560-01-518-9434 Item PartTypeName: PANEL,STRUCTURAL,AIRCRAFT | 1560 | 015189434 | 0 | P | A | |
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
U | A | A | 0 | |||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
17P2A5204-2 | 6 | 2 | 3 |
MRC | Criteria | Characteristic |
---|---|---|
SR-5 | Design Control Reference Or Manufacturers Code | |
ABHP | Overall Length | 23.000 INCHES NOMINAL |
SR-5 | Design Control Reference Or Manufacturers Code | 88277 |
CZEJ | Aircraft Station Number | FY 1137.500 TO FY1160.500 |
SR-5 | Design Control Reference Or Manufacturers Code | 17P2A5204-2 |
FEAT | Special Features | NHA 7P2A5618-514; EFFECTIVITY FROM 17A103-184; PLATE, HEAT TREAT T7451 |
CZEK | Aircraft Mission Design Series | C-17A |
MATT | Material | ALUMINUM ALLOY 7075 |
CZDJ | Aircraft Location | MLG POD |
MRC | Decoded Requirement | Clear Text Reply |
CXCY | Part Name Assigned By Controlling Agency | PLATFORM,STRUCTURAL |
ABNM | Thickness | 1.750 INCHES NOMINAL |
ABMK | Overall Width | 22.000 INCHES NOMINAL |
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