INSTANT RFQ

Complete Listing of NSN (9535015317781) Parts 9535-01-531-7781

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) 01-531-7781 (015317781)
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-T3-0.032X12X48 society of automotive engineers inc sheet metal 81343 RFQ
AMS QQ A 250 5 sae international sheet metal 0u583 RFQ
AMS-QQ-A-250 5 society of automotive engineers inc sheet metal 81343 RFQ
AMS QQ A 250 5 T3 0 032X12X48 sae international sheet metal 0u583 RFQ
AMS-QQ-A-250 5-CDT3-0 032X12X48 society of automotive engineers inc sheet metal 81343 RFQ

Technical Characteristics of NSN 9535015317781

MRCCriteriaCharacteristic
AARNFABRICATION METHODROLLED
ABGLWIDTH12.000 INCHES NOMINAL
ABRYLENGTH48.000 INCHES NOMINAL
ADVMCROSS-SECTIONAL THICKNESS0.0320 INCHES NOMINAL
AGAVEND ITEM IDENTIFICATIONFUSELAGE F4F JET AIRCRAFT
AGTABASIC SHAPE STYLESOLID
ALBYUSAGE DESIGNAIRCRAFT
CQBCMINIMUM TENSILE STRENGTH59000 POUNDS PER SQUARE INCH
CQHQMINIMUM YIELD STRENGTH39000 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 5.0 PERCENT OF COMPOSITE THICKNESS OR 4.0 PERCENT OF FINISHED SHEET THICKNESS
HEATHEAT TREATMENTT-3 SOLUTION HEAT TREATED
MATLMATERIALALUMINUM ALLOY, QQ-A-250/5
AARNFABRICATION METHODROLLED
ABGLWIDTH12.000 INCHES NOMINAL
ABRYLENGTH48.000 INCHES NOMINAL
ADVMCROSS-SECTIONAL THICKNESS0.0320 INCHES NOMINAL
AGAVEND ITEM IDENTIFICATIONFUSELAGE F4F JET AIRCRAFT
AGTABASIC SHAPE STYLESOLID
ALBYUSAGE DESIGNAIRCRAFT
CQBCMINIMUM TENSILE STRENGTH59000 POUNDS PER SQUARE INCH
CQHQMINIMUM YIELD STRENGTH39000 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 5.0 PERCENT OF COMPOSITE THICKNESS OR 4.0 PERCENT OF FINISHED SHEET THICKNESS
HEATHEAT TREATMENTT-3 SOLUTION HEAT TREATED
MATLMATERIALALUMINUM ALLOY, QQ-A-250/5

Relevant Components for NSN - 9535-01-531-7781, 9535015317781
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