At Orbit NSN, we offer an expansive inventory of Panel Structural Aircraft components by Boeing Company The, including part number 17P2A6011-6, and many others. On this page, you can complete and submit a quote request form for this part number and others with the NSN 1560013704092 to receive a customized solution within 15 minutes or less of submission. All we ask is that you include relevant information while filling out this form, such as your desired part quantity and budget parameters, so our dedicated staff can best respond with a quote that suits your needs and restrictions alike.
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Quality is the cornerstone of our operations at Orbit NSN, and as such, we proudly operate with AS9120B, ISO 9001:2015, and FAA AC 00-56B accreditation, in addition to adhering to a strict NO CHINA SOURCING policy. To make your search simple, our catalogs feature items with CAGE Code 88277 and FSC 1560 Airframe Structural Components so that you always know you are procuring the exact items you need. To learn more about components with the NSN 1560-01-370-4092, such as this part manufactured by Boeing Company The, give us a call or email at any time, and a dedicated team member will be more than happy to assist you however they can through the procurement process. Get started today to see why our customers continue to rely on our top-notch products and services for all their operational needs.
NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
1560-01-370-4092 Item PartTypeName: 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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