You are currently exploring our in-stock options for part number AMS QQ A 250 5 with the NSN 9535015317789. This product is listed with the description “Sheet Metal” and is manufactured by Sae International. If you are looking to purchase this part, we encourage you to complete and submit the RFQ form below with as much information as you can provide, such as your desired quantity, budget, shipping time frame, and more. Within 15 minutes of receiving and reviewing your submission, one of our experts will reach out with a quote that is tailored to your needs.
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We supply all relevant information alongside the listings on our website, that way you know you are always getting the exact item you require. For example, part number AMS QQ A 250 5 is listed alongside the NSN 9535-01-531-7789 and belongs to the FSC 9535 Plate Sheet Strip and Foil Nonferrous Base Metal. Additionally, it is also under the CAGE Code 0U583, which is assigned to Sae International. At Aerospace Procurement, you can trust that each product in our inventory is up to industry standards, as we are committed to various quality assurance practices. For example, we uphold a strict NO CHINA SOURCING pledge to ensure that each part is shipped out alongside its manufacturer trace documentation and qualifying certifications. These practices and more allow us to operate with AS9120B, ISO 9001:2015, and FAA AC 00-56B accreditation. Get in contact with us today to see how we can make the procurement process for part number AMS QQ A 250 5 seamless.
NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
9535-01-531-7789 Item PartTypeName: SHEET,METAL | 9535 | 015317789 | N | A | ||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
A | A | 0 | ||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
AMS-QQ-A-250/5-CDT3-0,04X6X36 | 5 | 9 | 5 |
MRC | Criteria | Characteristic |
---|---|---|
MATT | Material | ALUMINUM ALLOY 2024 |
MDCL | Material Document And Classification | QQ-A-250/5 FED SPEC 1ST MATERIAL RESPONSE |
CQHQ | Minimum Yield Strength | 39000 POUNDS PER SQUARE INCH |
AGTA | Basic Shape Style | SOLID |
ABRY | Length | 36.000 INCHES NOMINAL |
HEAT | Heat Treatment | T-3 SOLUTION HEAT TREATED |
AGAV | End Item Identification | FUSELAGE F4F JET AIRCRAFT |
ABGL | Width | 6.000 INCHES NOMINAL |
CQBC | Minimum Tensile Strength | 59000 POUNDS PER SQUARE INCH |
MRC | Decoded Requirement | Clear Text Reply |
ALBY | Usage Design | AIRCRAFT |
FEAT | Special Features | THIN LAYERS APPROXIMATELY EQUAL THICKNESS, OF ALUMINUM ALLOY 1230 ANODIC TO THE CORE ARE BONDED TO BOTH SURFACES; NOMINAL CLADDING THICKNESS FOR EACH LAYER TO BE 5.0 PERCENT OF COMPOSITE THICKNESS OR 4.0 PERCENT OF FINISHED SHEET THICKNESS |
AARN | Fabrication Method | ROLLED |
ADVM | Cross-Sectional Thickness | 0.0400 INCHES NOMINAL |
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