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 L3223760-077, a Boeing Company The item with the NSN 1560014496570 that is listed alongside the description “Panel Structural Aircraft.” If you are interested in part number L3223760-077 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 L3223760-077 is specifically listed with the NSN 1560-01-449-6570, 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 43999. With our services and dedication to simple procurement in mind, get started with us today!
NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
1560-01-449-6570 Item PartTypeName: PANEL,STRUCTURAL,AIRCRAFT | 1560 | 014496570 | 0 | P | ||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
7 | A | 0 | ||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
L3223760-077 | 6 | 2 | 3 |
MRC | Criteria | Characteristic |
---|---|---|
MATT | Material | ALUMINUM ALLOY 2024 |
ABMK | Overall Width | 8.000 INCHES NOMINAL |
MDCL | Material Document And Classification | QQ-A-250/5 FED SPEC SINGLE MATERIAL RESPONSE |
CZEK | Aircraft Mission Design Series | B-1B |
MRC | Decoded Requirement | Clear Text Reply |
FEAT | Special Features | NNUCLEAR HARDNESS CRITICAL ITEM; MANUFACTURER SUGGESTED NAME-PANEL, WEDGE, PIVOTING-UNDERWING FARING; NHA -001 ASSY; HEAT TREAT TO COND T62 PER ST0111LA0009; FINISH 11AB02; MATL: AL CLAD SH; 0 TEMPER; OPPOSITE -078 |
NHCF | Nuclear Hardness Critical Feature | HARDENED |
ABNM | Thickness | 0.063 INCHES NOMINAL |
ABHP | Overall Length | 15.700 INCHES NOMINAL |
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