Mfg Part Number: AMS-QQ-A-250 5 | Alternate P/N: AMSQQA2505 | Manufacturer: Society Of Automotive Engineers Inc |
NSN : 9535-01-531-7794 | NIIN : 015317794 | Item Name : sheet metal |
CAGE Code : 81343 | FSC : 9535 Plate Sheet Strip and Foil Nonferrous Base Metal |
When you need NSN parts bolstered by rapid lead times and cost savings along all avenues, call on Aviation Parts Distributor to get the job done. Here, entities can request a quote for any AMS-QQ-A-250 5 (Sheet Metal) product of interest associated with the NSN 9535-01-531-7794, by Society Of Automotive Engineers Inc, those of which are housed on our online database of over 2 billion new, used, obsolete, and hard-to-find NSN components. Readily available for purchase through the submission of an RFQ form as provided on this page, entities may request a quote for their comparisons on desired NSN items with the part number AMS-QQ-A-250 5 that are of interest. Upon receiving a completed RFQ form, our account representatives will utilize their market prowess to provide you with a solution that satisfies your part needs in just 15 minutes or less.
Operating as an FAA AC 00-56B, AS9120B, and ISO 9001:2015 accredited enterprise, our customers can trust in the quality of our processes. As the only independent distributor with a NO CHINA SOURCING pledge, we guarantee the authenticity of all purchased parts, meaning that all items are shipped alongside their manufacturer trace documentation or qualifying certifications, as applicable. With our global supply chain stretching across the United States, customers can experience little operational downtime when requesting customized shipping on AMS-QQ-A-250 5 (9535-01-531-7794) items with the CAGE Code 81343, by Society Of Automotive Engineers Inc.
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 | END ITEM IDENTIFICATION | FUSELAGE F4F JET AIRCRAFT |
AGTA | BASIC SHAPE STYLE | SOLID |
ALBY | 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 |
MATL | MATERIAL | ALUMINUM ALLOY, QQ-A-250/5 |
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 | END ITEM IDENTIFICATION | FUSELAGE F4F JET AIRCRAFT |
AGTA | BASIC SHAPE STYLE | SOLID |
ALBY | 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 |
MATL | MATERIAL | ALUMINUM ALLOY, QQ-A-250/5 |
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