We appreciate your interest in our selection of parts that fall under the NSN 9535-01-531-7795. Below, top-requested part numbers like AMS-QQ-A-250 5-T81-0.040X12X36, AMS-QQ-A-250 5-CDT81-0 04X12X36, AMS-QQ-A-250 5, and others are presented alongside their manufacturer for your perusal. In order to receive pricing options on any featured NSN 9535-01-531-7795, simply click on the “RFQ” button next to it and complete the quote request form you are directed to. Be sure to include as many details as you can about your requirements and restrictions alike so our team can best formulate ideal fulfillment options for your consideration.
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Item Name | Sheet Metal |
Federal Supply Group (FSG) | Metal Bars Sheets and Shapes |
Federal Supply Class (FSC) | 9535 Plate Sheet Strip and Foil Nonferrous Base Metal |
National Item Identification Number (NIIN) | 01-531-7795 (015317795) |
NCB Code | USA (01) |
Manufacturer | Sae International, Society Of Automotive Engineers Inc |
Part Number | Manufacturer | Item Name | RFQ |
---|---|---|---|
AMS-QQ-A-250 5-T81-0.040X12X36 | sae international | sheet metal | RFQ |
AMS-QQ-A-250 5-CDT81-0 04X12X36 | society of automotive engineers inc | sheet metal | RFQ |
AMS-QQ-A-250 5-T81-0.040X12X36 | society of automotive engineers inc | sheet metal | RFQ |
AMS-QQ-A-250 5 | society of automotive engineers inc | sheet metal | RFQ |
AMS-QQ-A-250 5 | sae international | sheet metal | RFQ |
MRC | Criteria | Characteristic |
---|---|---|
AARN | FABRICATION METHOD | ROLLED |
ABGL | WIDTH | 12.000 INCHES NOMINAL |
ABRY | LENGTH | 36.000 INCHES NOMINAL |
ADVM | CROSS-SECTIONAL THICKNESS | 0.0400 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 |
CQHQ | MINIMUM YIELD STRENGTH | 54000 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 5.0 PERCENT OF COMPOSITE THICKNESS OR 4.0 PERCENT OF FINISHED SHEET THICKNESS |
HEAT | HEAT TREATMENT | T-81 SOLUTION HEAT TREATED |
MATL | MATERIAL | ALUMINUM ALLOY, QQ-A-250/5 |
AARN | FABRICATION METHOD | ROLLED |
ABGL | WIDTH | 12.000 INCHES NOMINAL |
ABRY | LENGTH | 36.000 INCHES NOMINAL |
ADVM | CROSS-SECTIONAL THICKNESS | 0.0400 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 |
CQHQ | MINIMUM YIELD STRENGTH | 54000 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 5.0 PERCENT OF COMPOSITE THICKNESS OR 4.0 PERCENT OF FINISHED SHEET THICKNESS |
HEAT | HEAT TREATMENT | T-81 SOLUTION HEAT TREATED |
MATL | MATERIAL | ALUMINUM ALLOY, QQ-A-250/5 |
Relevant Components for NSN - 9535-01-531-7795, 9535015317795 | ||||
9535-01-533-6174 (9535015336174) | 9510-01-204-1154 (9510012041154) | 9530-01-369-7643 (9530013697643) | 9530-01-262-8756 (9530012628756) | |
9530-01-262-8869 (9530012628869) | 9520-00-203-1806 (9520002031806) | 9540-01-209-3173 (9540012093173) | 9530-01-497-1215 (9530014971215) | |
9535-00-954-2630 (9535009542630) | 9515-00-950-2593 (9515009502593) | 9510-00-541-9655 (9510005419655) | 9515-00-580-5680 (9515005805680) | |
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