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Quality guaranteed We sell only warrantied and traceable partsThank you for your interest in 17P2A6011 5 available NSN part on NSN Sphere. Panel Structural Ai is listed with the part number 17P2A6011 5, and its manufacturer is Boeing Company The. This NSN part is currently available for purchase through our website today, and you may begin the process by filling out the following RFQ form. By providing us with information such as what parts you need, when you need them by, and your target price, our team can present you with a personalized quote that has been specifically tailored to fit your individual needs and requirements. Once you have submitted your request, a dedicated account manager will review and reach out to you in 15 minutes or less to continue the purchasing process.
As a leading online distributor of NSN parts like 17P2A6011 5, we provide customers access to an expansive database of new, used, and obsolete items that have been sourced from top global manufacturers such as Boeing Company The. If you are facing an AOG situation or time constraint, we provide same-day delivery and expedited shipping on a number of items. Get started on the purchasing process for NSN 1560013704087 under FSC 1560 Airframe Structural Components and experience how NSN Sphere can serve as your strategic sourcing partner for all of your operational needs.
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 1560-01-370-4087 Item Description: Panel Structural Ai | 1560 | 013704087 | 0 | P | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| U | A | 0 | ||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| 17P2A6011 5 | 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 | 17P2A6011-215 |
| 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 981.500 |
| FEAT | Special Features | NHA 17P2A6011-213;PANEL INSTL-FILLET,LWR Y=910.500 THRU Y=981.500 |
| MATT | Material | PLASTIC POLYAMIDE AND |
| MDCL | Material Document And Classification | DMS2502 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 | LEFT SIDE |
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