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 17P2A6022-6, which is a Panel Structural Aircraft item from Boeing Company The that is listed with the NSN 1560-01-370-3642 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 17P2A6022-6 was specifically produced by Boeing Company The under the CAGE Code 88277, providing traceability. Furthermore, with the NSN 1560-01-370-3642, 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 17P2A6022-6, and we will be in touch.
NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
1560-01-370-3642 Item PartTypeName: PANEL,STRUCTURAL,AIRCRAFT | 1560 | 013703642 | 0 | P | ||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
U | A | 0 | ||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
17P2A6022-6 | 6 | 2 | 3 |
MRC | Criteria | Characteristic |
---|---|---|
SFTT | Surface Treatment | PRIMER EPOXY |
MRC | Decoded Requirement | Clear Text Reply |
SR-5 | Design Control Reference Or Manufacturers Code | 17P2A6022-6 |
MDCL | Material Document And Classification | DMS1974 MFR REF 1ST MATERIAL RESPONSE AND |
SR-5 | Design Control Reference Or Manufacturers Code | |
CZDJ | Aircraft Location | CENTER FUSELAGE,WING FILLET,CLOSEOUT |
SR-5 | Design Control Reference Or Manufacturers Code | 88277 |
MDCL | Material Document And Classification | DMS2288 MFR REF 2ND MATERIAL RESPONSE |
CZEK | Aircraft Mission Design Series | C-17A |
STDC | Surface Treatment Document And Classification | MIL-P-23377 MIL SPEC 1ST TREATMENT RESPONSE AND |
CZEJ | Aircraft Station Number | FS 981.500 TO FS 1045.75 |
FEAT | Special Features | NHA 17P2A6022-4;PANEL INSTL,FILLET CLOSEOUT-Y=981.50 TO Y=1045.75 |
STDC | Surface Treatment Document And Classification | MIL-F-18264 MIL SPEC 2ND TREATMENT RESPONSE |
MATT | Material | PLASTIC POLYAMIDE AND |
AARN | Fabrication Method | COMPOSITE |
AARN | Fabrication Method | LAMINATED AND |
MATT | Material | PLASTIC ARAMID |
BWJF | Side For Which Designed | RIGHT SIDE |
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