Thank you for taking an interest in the top-caliber NSN products we feature here on AI NSN Parts. On this page, you can submit a quote request for part number DAA3132D902-011, a Panel Structural Aircraft item that is manufactured by The Boeing Company. Listed alongside the NSN 1560014697475 within our database, part number DAA3132D902-011 is conveniently ready for purchase at any time.
To ensure listings like part number DAA3132D902-011 are ready for swift installation, we have a rigorous quality assurance program in place. As such, we make it easy for you to inquire about popular NSNs like 1560-01-469-7475, as well as the many other The Boeing Company products produced under CAGE Code 81205 that interest you. For the benefit of our customers, we carefully vet every entity that we source from, guaranteeing that you only receive superior-caliber offerings in every order. With these dedications, you can always purchase from us with confidence. Furthermore, we also organize our stock based on Federal Supply Classes, so you can find popular items under FSCs like 1560 Airframe Structural Components. Do not hesitate to submit the RFQ form below, and within 15 minutes or less of submission, one of our experts will reach out with a customized solution. Get started today and see why so many customers steadily depend on AI NSN Parts for their operational needs.
NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
1560-01-469-7475 Item PartTypeName: PANEL,STRUCTURAL,AIRCRAFT | 1560 | 014697475 | 0 | P | ||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
7 | A | 0 | ||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
DAA3132D902-011 | 6 | 2 | 3 |
MRC | Criteria | Characteristic |
---|---|---|
NHCF | Nuclear Hardness Critical Feature | HARDENED |
CRTL | Criticality Code Justification | FEAT |
CZEK | Aircraft Mission Design Series | B-2 PACER SPECIAL |
MATT | Material | PLASTIC ARAMID |
FEAT | Special Features | NHA DAA3132B900;EFFECTIVITY R0017-R09999;OPPOSITE -012;NUCLEAR HARDNESSCRITCAL ITEM AND SMOOTHNESS CRITICAL ITEM;C/O 5 CORE (-013, -015, -017, -019, -023);NOMEX HONEYCOMB CORE PER BMS8-124 CLASS IV, TYPE V, GRADE 8;THKNESS TOLERANCE PLUS OR MINUS .006;FINISH F-14.67 PLUS F-19.62 HCP EXCEPT BAG SIDEFINISH |
MRC | Decoded Requirement | Clear Text Reply |
CZDJ | Aircraft Location | OUTBOARD UPPER TRAILING EDGE PANEL ASSEMBLY |
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