INSTANT RFQ

Complete Listing of NSN (9535015317800) Parts 9535-01-531-7800

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 Society Of Automotive Engineers Inc, Sae International
Part Number Manufacturer Item Name Cage Code RFQ
AMS-QQ-A-250-5-T351-1-000X6X24 society of automotive engineers inc plate metal 81343 RFQ
AMS-QQ-A-250 5 society of automotive engineers inc plate metal 81343 RFQ
AMS-QQ-A-250 5-CDT351-1 0X6X24 society of automotive engineers inc plate metal 81343 RFQ
AMS-QQ-A-250 5 sae international plate metal 0u583 RFQ
AMS-QQ-A-250 5-T351-1.000X6X24 sae international plate metal 0u583 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
9515-01-536-3375 (9515015363375) 9515-00-814-7221 (9515008147221) 9530-00-237-0734 (9530002370734) 9540-00-197-9847 (9540001979847)
9520-01-274-4554 (9520012744554) 9515-00-061-4892 (9515000614892) 9530-01-135-8297 (9530011358297) 9535-01-581-6877 (9535015816877)
9510-00-541-9207 (9510005419207) 9540-01-071-2142 (9540010712142) 9530-00-060-5585 (9530000605585) 9530-00-233-1340 (9530002331340)

Submit a Quote and We'll Get Back to You Shortly

Guaranteed quotes back within 15 minutes, 24/7 x 365

Thank You for Visiting.

If You’re Ever Looking for NSN parts Or Have an Aircraft On Ground Situation, Don’t forget That We offer Competitive Pricing and Guaranteed On-Time Delivery.

Request for Quote

We use cookies to ensure that we give you the best experience on our website. If you continue to use this site we will assume that you are happy with it.

bottom to top