We are pleased to offer procurement for Society Of Automotive Engineers Inc part number AMS-QQ-A-250 8-CDH34-0 04X12X48 here on NSN Portal, a Sheet Metal product that is listed with the NSN 9535-01-532-0513 for ease of identification. You have reached our Request for Quote (RFQ) form for this listing, where you are encouraged to submit details on your requirements to receive tailored purchasing options from our staff. As you will see, we ask that you offer key information on your pricing target, desired quantity, and more, as this will ensure that the representative who responds to your request is able to provide the most fitting solutions for your needs.
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Whether you procure part number AMS-QQ-A-250 8-CDH34-0 04X12X48 or other NSN products from our website, you can rest assured that we uphold full traceability for all items. For example, this particular listing traces back to Society Of Automotive Engineers Inc through the CAGE Code 81343, as well as falls under FSC 9535 Plate Sheet Strip and Foil Nonferrous Base Metal based on having the NSN 9535-01-532-0513. Furthermore, every purchase will be delivered with any applicable qualifying certifications or manufacturer trace documentation as per our NO CHINA SOURCING pledge. If you are ready to experience why professionals rely on us for their needs, request a quote for part number AMS-QQ-A-250 8-CDH34-0 04X12X48 today and take advantage of our industry-leading services.
NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
9535-01-532-0513 Item PartTypeName: SHEET,METAL | 9535 | 015320513 | N | A | ||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
A | A | 0 | ||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
AMS-QQ-A-250/8-H34-0.040X12X48 | 5 | 2 | 3 |
MRC | Criteria | Characteristic |
---|---|---|
ADVM | Cross-Sectional Thickness | 0.0400 INCHES NOMINAL |
MATT | Material | ALUMINUM ALLOY 5052 |
HEAT | Heat Treatment | H-34 STRAIN HARDENED |
AGTA | Basic Shape Style | SOLID |
ABRY | Length | 48.000 INCHES NOMINAL |
ABGL | Width | 12.000 INCHES NOMINAL |
AGAV | End Item Identification | FUSELAGE, F4F JET AIRCRAFT |
CQBC | Minimum Tensile Strength | 34000 POUNDS PER SQUARE INCH |
MDCL | Material Document And Classification | QQ-A-250/8 FED SPEC 1ST MATERIAL RESPONSE |
ALBY | Usage Design | AIRCRAFT |
MRC | Decoded Requirement | Clear Text Reply |
FEAT | Special Features | MAXIMUM TENSILE STRENGTH 41000.0 POUNDS PER SQUARE INCH |
AARN | Fabrication Method | ROLLED |
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