Mfg Part Number: 17P2A6011-215 | Alternate P/N: 17P2A6011215 | Manufacturer: The Boeing Company |
NSN : 1560-01-370-4087 | Item Name : panel structural ai | CAGE Code : 88277 |
FSC : 1560 Airframe Structural Components |
Thank you for your interest in NSN 1560-01-370-4087 manufactured by The Boeing Company. The particular NSN product you are looking for is listed alongside the part number 17P2A6011-215, and is described as Panel Structural Ai. As we have this item available, we invite you to request a quote for your comparisons by filling out our RFQ form below. Once you have completed our form, we ask that you provide us with details regarding target prices, quantities, and expected shipping time frame. In this way, we can provide you with a quote that meets your specifications and requirements.
Beyond NSN 1560-01-370-4087 manufactured under CAGE Code 88277, and other various The Boeing Company parts, Acquire NSN has a stock inventory of over 2 billion new, used, obsolete, and hard-to-find NSN parts 17P2A6011-215 that work to meet the needs of a variety of industry verticals and applications. Acquire NSN operates under AS9120B and ISO 9001:2015 certification and FAA AC 00-56B accreditation to ensure the quality and authenticity of our offerings. We have developed an interface that simplifies the purchasing process with rapid response times for the industries we serve. Get started on the procurement process today and see why customers steadily rely on Acquire NSN for all their 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 |
17p2a6011-215 | 6 | 2 | 3 |
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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