NSN 9540-01-353-5555, (9540013535555) Beam Structural Parts

The NSN 9540-01-353-5555 part numbers 60-685, 4E117, AMS-QQ-A-200 3, QQ A 200 3 manufactured by Transtar Metals Corp, Boeing Company, Sae International, Society Of Automotive Engineers Inc, Federal Specifications Promulgat is available in our inventory. As an ASAP Semiconductor owned and operated website, ASAP Aviation Unlimited has access to over three billion parts, paired with easy-to-use search engines that enable our customers to browse through our NSN 9540-01-353-5555 inventory quickly and efficiently. Our focus on quality control has earned us our FAA AC 0056B accreditation and AS9120B, ISO 9001:2015 certification, and we are the only independent distributor with a No China Sourcing pledge. If you are ready to get started, you can send an Instant RFQ form from this page for NSN 9540-01-353-5555 parts of Beam Structural, and one of our account managers will respond to it within fifteen minutes or less.


Alternative NSN: 9540-01-353-5555
Item Name: Beam Structural
FSG: 95 Metal Bars Sheets and Shapes
Federal Supply Class (FSC): 9540 Structural Shapes Nonferrous Base Metal
NIIN: 013535555
NCB Code: USA (01)

Part Number's List for NSN 9540-01-353-5555, 9540013535555

Part No Manufacturer Item Name QTY RFQ
60-685 transtar metals corp beam structural Avl RFQ
4E117 boeing company beam structural Avl RFQ
AMS-QQ-A-200 3 sae international beam structural Avl RFQ
AMS-QQ-A-200 3 society of automotive engineers inc beam structural Avl RFQ
QQ A 200 3 federal specifications promulgat beam structural Avl RFQ

Technical Characteristics of NSN 9540013535555

MRCCriteriaCharacteristic
ABRYLENGTH12.000 FEET NOMINAL
ADXSRIGHT SIDE TOP FLANGE THICKNESS0.062 INCHES NOMINAL
AJJBFIRST TIP RADIUS0.031 INCHES NOMINAL
AJJPLEG THICKNESS0.062 INCHES NOMINAL
BPXGRIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES0.875 INCHES NOMINAL
BPXLFILLET RADIUS WHERE TOP RIGHT FLANGE JOINS WEB FLANGE/LEG0.094 INCHES NOMINAL
BRFDWEIGHT PER UNIT MEASURE0.203 POUNDS PER LINEAR FOOT
CNQJSECOND TIP RELATIONSHIP TO FIRST TIPIDENTICAL
CSMZLEFT TOP INSIDE ANGLE90.0 DEGREES NOMINAL
HEATHEAT TREATMENTT-8511 SOLUTION HEAT TREATED
MATLMATERIALALUMINUM ALLOY, QQ-A-200/3
MATTMATERIALALUMINUM ALLOY 2024
AARNFABRICATION METHODEXTRUDED
ABKWOVERALL HEIGHT1.000 INCHES NOMINAL
ADXRLEFT SIDE TOP FLANGE THICKNESS0.062 INCHES NOMINAL
AGTABASIC SHAPE STYLET SHAPE
BPXDLEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES0.875 INCHES NOMINAL
BPXJFILLET RADIUS WHERE TOP LEFT FLANGE JOINS WEB FLANGE/LEG0.094 INCHES NOMINAL
BQJGTOP FLANGE WIDTH1.750 INCHES NOMINAL
CMZYFIRST TIP STYLEFULL RADIUS
CNQLTHIRD TIP RELATIONSHIP TO PRECEDING TIPSIDENTICAL W/FIRST TIP
CRZCRIGHT TOP INSIDE ANGLE90.0 DEGREES NOMINAL
MDCLMATERIAL DOCUMENT AND CLASSIFICATIONQQ-A-200/3 FED SPEC 1ST MATERIAL RESPONSE
ZZZTNONDEFINITIVE SPEC/STD DATAT8511 TEMPER

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