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We have a large inventory from top manufacturers such as Sae International, Society Of Automotiv, Society Of Automotive Engineers Inc with top products such as AMS-QQ-A-250 5, AMS-QQ-A-250 5-T351-1.000X6X24, AMS-QQ-A-250-5, AMS-QQ-A-250-5-CDT351-1 0X6X24, AMS-QQ-A-250-5-CDT351-1-0X6X24 for NSN 9535-01-531-7800 Plate Metal Parts. We pride ourselves on serving the U.S. and her allies while maintaining our No China Sourcing Policy. We invite you to explore our NSN parts at your leisure, and our team of industry experts are on standby to assist you through the purchasing process as needed. Fill out the request for quote form below and hear from a dedicated account representative in fifteen minutes.
Part Information of NSN 9535015317800
Part No | Manufacturer | Item Name | QTY | RFQ |
---|---|---|---|---|
AMS-QQ-A-250 5 | sae international | plate metal | Avl | RFQ |
AMS-QQ-A-250 5-T351-1.000X6X24 | sae international | plate metal | Avl | RFQ |
AMS-QQ-A-250-5 | society of automotiv | plate metal | Avl | RFQ |
AMS-QQ-A-250-5-CDT351-1 0X6X24 | society of automotive engineers inc | plate metal | Avl | RFQ |
AMS-QQ-A-250-5-CDT351-1-0X6X24 | society of automotiv | plate metal | Avl | RFQ |
AMS-QQ-A-250-5-T351-1-000X6X24 | society of automotiv | plate metal | Avl | RFQ |
AMS-QQ-A-250-5-T351-1-000X6X24 | society of automotive engineers inc | plate metal | Avl | RFQ |
Product Details of NSN 9535015317800
MRC | Criteria | Characteristic |
---|---|---|
MATL | MATERIAL | ALUMINUM ALLOY, QQ-A-250/5 |
CQHQ | MINIMUM YIELD STRENGTH | 42000 POUNDS PER SQUARE INCH |
AARN | FABRICATION METHOD | ROLLED |
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 PLATE THICKNESS |
ADVM | CROSS-SECTIONAL THICKNESS | 1.0000 INCHES NOMINAL |
ABGL | WIDTH | 6.000 INCHES NOMINAL |
ABRY | LENGTH | 24.000 INCHES NOMINAL |
AGAV | END ITEM IDENTIFICATION | FUSELAGE F4F JET AIRCRAFT |
AGTA | BASIC SHAPE STYLE | SOLID |
ALBY | USAGE DESIGN | AIRCRAFT |
CQBC | MINIMUM TENSILE STRENGTH | 62000 POUNDS PER SQUARE INCH |
HEAT | HEAT TREATMENT | T-351 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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