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 520-18824-10, a Nordam Group Inc item with the NSN 1560016470132 that is listed alongside the description “Plate Structural Aircraft.” If you are interested in part number 520-18824-10 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 520-18824-10 is specifically listed with the NSN 1560-01-647-0132, and this code can be used to determine that it falls under FSC 1560 Airframe Structural Components. Additionally, while tracing back to Nordam Group Inc, this NSN part was specifically produced under CAGE Code 29957. With our services and dedication to simple procurement in mind, get started with us today!
NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
1560-01-647-0132 Item PartTypeName: PLATE,STRUCTURAL,AIRCRAFT | 1560 | 016470132 | 0 | P | A | |
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
U | A | A | 0 | |||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
520-18824-10 | 5 | 2 | 5 |
MRC | Criteria | Characteristic |
---|---|---|
ABHP | OVERALL LENGTH | 20.0 INCHES NOMINAL |
ABMK | OVERALL WIDTH | 1.0 INCHES NOMINAL |
ABPX | MATERIAL THICKNESS | 0.090 INCHES NOMINAL |
AGAV | III END ITEM IDENTIFICATION | B-52 ACFT |
CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | OUTBOARD SPLICE ANGLE |
CZEK | AIRCRAFT MISSION DESIGN SERIES | B52 |
FEAT | SPECIAL FEATURES | OUTBOARD SPLICE ANGLE;AFT WHEEL WELL;NEXT HIGHER ASSEMBLY 520-18822;PENETRANT INSPECT PER MIL-STD-1907, GRADE A(BAC 5423 IS MANDATORY FOR INTERNAL USE BY BOEING AND THEIR CUBCONTRACTORS.) |
MATT | III MATERIAL | ALUMINUM ALLOY 7075 |
MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | AMS-QQ-A-250/13 ASSN STD SINGLE MATERIAL RESPONSE |
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