Thank you for taking interest in the Boeing Company The part number 17P2A6011-5, a Panel Structural Aircraft product that we stock that is presented alongside the NSN 1560-01-370-4087 for ease of identification. If you would like to learn more about this component and secure purchasing options for your consideration, please fill out and submit the Request for Quote (RFQ) form that is offered below. All we ask is that you supply us with enough information to best accommodate any particular requirements or restrictions that you may have, and we will respond with a curated quote within 15 minutes of our receipt and review.
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We strive to ensure that customers only receive precise items of need, opting to arrange our collection by diverse, commonly recognized forms of data. For instance, part number 17P2A6011-5 specifically traces back to Boeing Company The through the CAGE Code 88277, a distinct identifier for one of their physical locations. Moreover, with the NSN 1560-01-370-4087, this listing falls within Federal Supply Code (FSC) 1560 Airframe Structural Components, enabling one to figure out its basic application. Keeping this in mind, do not hesitate to obtain a competitive quote for part number 17P2A6011-5 here on Aero OEM Parts at your earliest convenience.
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 1560-01-370-4087 Item PartTypeName: PANEL,STRUCTURAL,AIRCRAFT | 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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