Database of Plate Metal Under NSN (9535015317800) 9535-01-531-7800 Parts

Item Name Plate 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) 01-531-7800 (015317800)
NCB Code USA (01)
Manufacturer Sae International, Society Of Automotive Engineers Inc
Part Number Manufacturer Item Name RFQ
AMS-QQ-A-250 5-T351-1.000X6X24 sae international plate metal RFQ
AMS-QQ-A-250 5-CDT351-1 0X6X24 society of automotive engineers inc plate metal RFQ
AMS-QQ-A-250-5-T351-1-000X6X24 society of automotive engineers inc plate metal RFQ
AMS-QQ-A-250 5 society of automotive engineers inc plate metal RFQ
AMS-QQ-A-250 5 sae international plate metal RFQ

Technical Characteristics of NSN 9535015317800

MRCCriteriaCharacteristic
AARNFABRICATION METHODROLLED
ABGLWIDTH6.000 INCHES NOMINAL
ABRYLENGTH24.000 INCHES NOMINAL
ADVMCROSS-SECTIONAL THICKNESS1.0000 INCHES NOMINAL
AGAVEND ITEM IDENTIFICATIONFUSELAGE F4F JET AIRCRAFT
AGTABASIC SHAPE STYLESOLID
ALBYUSAGE DESIGNAIRCRAFT
CQBCMINIMUM TENSILE STRENGTH62000 POUNDS PER SQUARE INCH
CQHQMINIMUM YIELD STRENGTH42000 POUNDS PER SQUARE INCH
FEATSPECIAL FEATURESTHIN 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
HEATHEAT TREATMENTT-351 SOLUTION HEAT TREATED
MATLMATERIALALUMINUM ALLOY, QQ-A-250/5
AARNFABRICATION METHODROLLED
ABGLWIDTH6.000 INCHES NOMINAL
ABRYLENGTH24.000 INCHES NOMINAL
ADVMCROSS-SECTIONAL THICKNESS1.0000 INCHES NOMINAL
AGAVEND ITEM IDENTIFICATIONFUSELAGE F4F JET AIRCRAFT
AGTABASIC SHAPE STYLESOLID
ALBYUSAGE DESIGNAIRCRAFT
CQBCMINIMUM TENSILE STRENGTH62000 POUNDS PER SQUARE INCH
CQHQMINIMUM YIELD STRENGTH42000 POUNDS PER SQUARE INCH
FEATSPECIAL FEATURESTHIN 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
HEATHEAT TREATMENTT-351 SOLUTION HEAT TREATED
MATLMATERIALALUMINUM ALLOY, QQ-A-250/5

Relevant Components for NSN - 9535-01-531-7800, 9535015317800
9540-01-018-7387 (9540010187387) 9510-00-583-5174 (9510005835174) 9520-00-071-4995 (9520000714995) 9535-00-221-2321 (9535002212321)
9510-00-231-2027 (9510002312027) 9540-01-525-0248 (9540015250248) 9515-01-562-3748 (9515015623748) 9540-00-487-5700 (9540004875700)
9515-00-206-8808 (9515002068808) 9515-01-622-2680 (9515016222680) 9520-00-277-4959 (9520002774959) 9510-00-256-6279 (9510002566279)

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