We appreciate your interest in Sae International part number AMS-QQ-A-250 8, which is currently ready for procurement here on Prompt Aerospace. For your reference, part number AMS-QQ-A-250 8 is listed with the NSN 9535-01-532-0507 and description “Sheet Metal.” If this is the item you are seeking and you would like to request a quote for your comparisons, simply complete the form below with information like your desired quantity, budget, and anticipated fulfillment timeframe. We regularly respond to requests within 15 minutes of receiving them, using the details we are offered to curate the most ideal purchasing options.
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If you want to explore other items produced by Sae International under the CAGE Code 0U583 or that similarly fall under the FSC 9535 Plate Sheet Strip and Foil Nonferrous Base Metal, keep in mind that since we list everything with relevant information, you can easily locate related part numbers using our search engine or catalogs. We also excel at tracking down parts with long lead times or that are generally hard to find, meaning that we can serve you even if you do not see exactly what you need on our website. With all of this being said, we are ready to help you source any of the NSN 9535-01-532-0507 parts and Sheet Metal items your operations require, so request a quote today.
NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
9535-01-532-0507 Item PartTypeName: SHEET,METAL | 9535 | 015320507 | N | A | ||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
A | A | 0 | ||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
AMS-QQ-A-250/8-H34-0.020X12X36 | 5 | 2 | 3 |
MRC | Criteria | Characteristic |
---|---|---|
MATT | Material | ALUMINUM ALLOY 5052 |
HEAT | Heat Treatment | H-34 STRAIN HARDENED |
AGTA | Basic Shape Style | SOLID |
ABRY | Length | 36.000 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 |
ADVM | Cross-Sectional Thickness | 0.0200 INCHES NOMINAL |
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