NSN - 9540-00-720-0685, 9540007200685 of Beam Structural

Aviation Axis stocks 19241, 60-9829, AMS QQ A 200 11, PA11369, QQ A 200 11 - Beam Structural made by Alcoa Reynolds Metals Company, Transtar Metals Corp, Society Of Automotive Engineers Inc, Sae International, Federal Specifications with 9540-00-720-0685. Owned and operated by ASAP Semiconductor, we have access to over 2 billion new and after-market parts applicable within the aerospace and defense industries. All our parts are shipped using our premier shipping and supply chain. We offer short lead-times and some of the fastest shipping times in the industry. We are well-equipped to handle any customer situation - including AOG. Submit an RFQ today and expect a response within 15 minutes or less. ASAP - the evolution of purchasing.

Part No Manufacturer Item Name QTY RFQ
19241 alcoa reynolds metals company beam structural Avl RFQ
60-9829 transtar metals corp beam structural Avl RFQ
AMS QQ A 200 11 society of automotive engineers inc beam structural Avl RFQ
AMS QQ A 200 11 sae international beam structural Avl RFQ
PA11369 transtar metals corp beam structural Avl RFQ
QQ A 200 11 federal specifications beam structural Avl RFQ
S6105-2076 sikorsky aircraft corporation beam structural Avl RFQ

Technical Characteristics of NSN 9540007200685

MRCCriteriaCharacteristic
AARNFABRICATION METHODEXTRUDED
ABKWOVERALL HEIGHT1.062 INCHES NOMINAL
ABRYLENGTH10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM
ADXSRIGHT SIDE TOP FLANGE THICKNESS0.050 INCHES NOMINAL
AGTABASIC SHAPE STYLET SHAPE
AJJPLEG THICKNESS0.050 INCHES NOMINAL
BPXDLEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES0.875 INCHES NOMINAL
BPXGRIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES0.875 INCHES NOMINAL
BPXJFILLET RADIUS WHERE TOP LEFT FLANGE JOINS WEB FLANGE/LEG0.062 INCHES NOMINAL
BPXLFILLET RADIUS WHERE TOP RIGHT FLANGE JOINS WEB FLANGE/LEG0.062 INCHES NOMINAL
BQJGTOP FLANGE WIDTH1.750 INCHES NOMINAL
BRFDWEIGHT PER UNIT MEASURE0.017 POUNDS PER LINEAR FOOT
CMZYFIRST TIP STYLESQUARE END
CNQLTHIRD TIP RELATIONSHIP TO PRECEDING TIPSIDENTICAL W/FIRST TIP
CRZCRIGHT TOP INSIDE ANGLE93.3 DEGREES NOMINAL
HEATHEAT TREATMENTT-6 SOLUTION HEAT TREATED
ZZZTNONDEFINITIVE SPEC/STD DATA7075 ALLOY AND T6 TEMPER
ADXRLEFT SIDE TOP FLANGE THICKNESS0.050 INCHES NOMINAL
CNQJSECOND TIP RELATIONSHIP TO FIRST TIPIDENTICAL
CSMZLEFT TOP INSIDE ANGLE86.3 DEGREES NOMINAL
MATTMATERIALALUMINUM ALLOY AMS-QQ-A-200/11, ALLOY 7075
SFTTSURFACE TREATMENTANODIZE

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