| Mfg Part Number: 17P2A6011-6 | Alternate P/N: 17P2A60116 | Manufacturer: Boeing Company |
| NSN : 1560-01-370-4092 | NIIN : 013704092 | Item Name : panel structural aircraft |
| CAGE Code : 88277 | FSC : 1560 Airframe Structural Components |
Thank you for choosing NSN Part 17P2A6011-6 of Hardware and Fasteners for all your operational needs. You have reached our NSN RFQ page which features all of our highly sought-after NSN 1560-01-370-4092 parts and components with Panel Structural Aircraft, manufactured by MFG Boeing Company. Some of these items include part 17P2A6011-6, and various others, all of which have been vetted for quality assurance and authenticity. At Hardware and Fasteners, we are committed to providing customers quality items that have been sourced from leading manufacturers across the globe. If you find yourself in need of quality parts and components, you have come to the right place.
17P2A6011-6 part of NSN 1560-01-370-4092 products that we feature by MFG Boeing Company are paired alongside CAGE Code 88277. Hardware and Fasteners uses CAGE Codes, allowing our customers to narrow down our vast catalogs with ease. When you find an item that works for your operations, fill out and submit an RFQ form for your comparisons. As you complete the form, please include target prices, desired quantities, and expected shipping time frames. Within 15 minutes of completion, an account manager will draft a sourcing solution that keeps your unique requirements in mind. Alternatively, you can call or email us directly; we are available 24/7x365!
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 1560-01-370-4092 Item Description: Panel Structural Aircraft | 1560 | 013704092 | 0 | P | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| U | A | 0 | ||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| 17p2a6011-6 | 6 | 1 | C | A |
| MRC | Criteria | Characteristic |
|---|---|---|
| SR-5 | Design Control Reference Or Manufacturers Code | |
| SFTT | Surface Treatment | PRIMER EPOXY |
| CZDJ | Aircraft Location | CENTER FUSELAGE FILLET,LOWER |
| MDCL | Material Document And Classification | DMS1974 MFR REF 1ST MATERIAL RESPONSE AND |
| SR-5 | Design Control Reference Or Manufacturers Code | 88277 |
| STDC | Surface Treatment Document And Classification | MIL-P-23377 MIL SPEC 1ST TREATMENT RESPONSE AND |
| SR-5 | Design Control Reference Or Manufacturers Code | 17P2A6011-216 |
| STDC | Surface Treatment Document And Classification | MIL-F-18264 MIL SPEC 2ND TREATMENT RESPONSE |
| MDCL | Material Document And Classification | DMS2288 MFR REF 3RD MATERIAL RESPONSE |
| CZEK | Aircraft Mission Design Series | C-17A |
| MATT | Material | PLASTIC ARAMID |
| MATT | Material | ALUMINUM ALLOY 1145 AND |
| CZEJ | Aircraft Station Number | FS 910.500 TO FS 918.500 |
| FEAT | Special Features | NHA 17P2A6011-214;PANEL INSTL-FILLET,LWR Y=910.500 THRU Y=981.500 |
| MATT | Material | PLASTIC POLYAMIDE AND |
| MDCL | Material Document And Classification | DMS2302 MFR REF 2ND MATERIAL RESPONSE AND |
| MRC | Decoded Requirement | Clear Text Reply |
| AARN | Fabrication Method | COMPOSITE |
| AARN | Fabrication Method | LAMINATED AND |
| BWJF | Side For Which Designed | RIGHT SIDE |
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