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Quality guaranteed We sell only warrantied and traceable partsThank you for your interest in AMS QQ A 250 5 available NSN part on NSN Sphere. Sheet Metal is listed with the part number AMS QQ A 250 5, and its manufacturer is Sae International. This NSN part is currently available for purchase through our website today, and you may begin the process by filling out the following RFQ form. By providing us with information such as what parts you need, when you need them by, and your target price, our team can present you with a personalized quote that has been specifically tailored to fit your individual needs and requirements. Once you have submitted your request, a dedicated account manager will review and reach out to you in 15 minutes or less to continue the purchasing process.
As a leading online distributor of NSN parts like AMS QQ A 250 5, we provide customers access to an expansive database of new, used, and obsolete items that have been sourced from top global manufacturers such as Sae International. If you are facing an AOG situation or time constraint, we provide same-day delivery and expedited shipping on a number of items. Get started on the purchasing process for NSN 9535015317794 under FSC 9535 Plate, Sheet, Strip, and Foil; Nonferrous Base Metal and experience how NSN Sphere can serve as your strategic sourcing partner for all of your operational needs.
| MRC | Criteria | Characteristic |
|---|---|---|
| AARN | FABRICATION METHOD | ROLLED |
| ABGL | WIDTH | 6.000 INCHES NOMINAL |
| ABRY | LENGTH | 36.000 INCHES NOMINAL |
| ADVM | CROSS-SECTIONAL THICKNESS | 0.0800 INCHES NOMINAL |
| AGAV | III END ITEM IDENTIFICATION | FUSELAGE F4F JET AIRCRAFT |
| AGTA | BASIC SHAPE STYLE | SOLID |
| ALBY | III USAGE DESIGN | AIRCRAFT |
| CQBC | MINIMUM TENSILE STRENGTH | 61000 POUNDS PER SQUARE INCH |
| CQHQ | MINIMUM YIELD STRENGTH | 40000 POUNDS PER SQUARE INCH |
| 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 2.5 PERCENT OF COMPOSITE THICKNESS OR 2.0 PERCENT OF FINISHED SHEET THICKNESS |
| HEAT | HEAT TREATMENT | T-3 SOLUTION HEAT TREATED |
| MATT | MATERIAL | ALUMINUM ALLOY 2024 |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/5 FED SPEC 1ST MATERIAL RESPONSE |
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