Thank you for taking an interest in the various military and defense parts, aerospace parts, and other items that we offer. You have reached the RFQ page for part number 17P2A6011-5, a Boeing Company The item with the NSN 1560013704087 that is listed alongside the description “Panel Structural Aircraft.” If you are interested in part number 17P2A6011-5 and wish to learn more about your purchasing options, be sure to submit the form below at your earliest convenience while supplying us with important information concerning your needs and restrictions alike. Once we have a chance to receive and review your completed form, a member of our staff will reach out to you in 15 minutes or less to present a tailored solution for your comparisons.
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To ensure that shopping with us is as simple as possible, we make it easy to identify and procure exact items by listing parts alongside all applicable designations and information. For example, part number 17P2A6011-5 is specifically listed with the NSN 1560-01-370-4087, and this code can be used to determine that it falls under FSC 1560 Airframe Structural Components. Additionally, while tracing back to Boeing Company The, this NSN part was specifically produced under CAGE Code 88277. With our services and dedication to simple procurement in mind, get started with us today!
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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