CVC10012-1002GA (Beam Structural) by Triumph Aerostructures Llc - Request a Quote Now

Part No. : CVC10012-1002GA Alternate P/N : CVC100121002GA Manufacturer : Triumph Aerostructures Llc
CAGE Code : 80378 Item Name : Beam Structural FSC : 9540 Structural Shapes Nonferrous Metal
NSN : 9540-01-430-2808

You can send a request for quote for p/n CVC10012-1002GA to ASAP Semiconductor using justpartsunlimited.com. This part is manufactured by Triumph Aerostructures Llc (CAGE Code 80378). The description of it is Beam Structural. The national stock number associated with this part is NSN 9540014302808. This part belongs to FSC Structural Shapes Nonferrous Metal part family. An associate from ASAP Semiconductor will respond within 15 minutes to your query. It is our pleasure to help you with CVC10012-1002GA part requirements.

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NSN Information for Part Number CVC10012-1002GA with NSN 9540-01-430-2808, 9540014302808

NSNFSCNIINCLSHazmatDEMILCancelled NSN
9540-01-430-2808

Item Description:

Beam Structural

95400143028080N
CIICHCCESDPMICCriticalityENAC
U A0
Part NumberISCRNVCRNCCHCCMSDSSADC
Cvc10012-1002ga523

Characteristics Data of NSN 9540-01-430-2808, 9540014302808

MRCCriteriaCharacteristic
AARNFABRICATION METHODEXTRUDED
ABKWOVERALL HEIGHT5.830 INCHES NOMINAL
ABRYLENGTH12.000 FEET NOMINAL
ADXRLEFT SIDE TOP FLANGE THICKNESS1.060 INCHES NOMINAL
ADXSRIGHT SIDE TOP FLANGE THICKNESS1.060 INCHES NOMINAL
AGAVEND ITEM IDENTIFICATIONB-2 BOMBER
AGTABASIC SHAPE STYLET SHAPE
AJJPLEG THICKNESS0.400 INCHES NOMINAL
BPXDLEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES1.810 INCHES NOMINAL
BPXGRIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES1.840 INCHES NOMINAL
BPXJFILLET RADIUS WHERE TOP LEFT FLANGE JOINS WEB FLANGE/LEG0.500 INCHES NOMINAL
BPXLFILLET RADIUS WHERE TOP RIGHT FLANGE JOINS WEB FLANGE/LEG0.500 INCHES NOMINAL
BQJGTOP FLANGE WIDTH3.650 INCHES NOMINAL
CMZYFIRST TIP STYLESQUARE W/ INNER AND OUTER CORNER RADII
CNBDFIRST TIP INNER RADIUS0.062 INCHES NOMINAL
CNBJFIRST TIP OUTER RADIUS0.062 INCHES NOMINAL
CNQJSECOND TIP RELATIONSHIP TO FIRST TIPIDENTICAL
CNQLTHIRD TIP RELATIONSHIP TO PRECEDING TIPSIDENTICAL W/FIRST TIP
CRZCRIGHT TOP INSIDE ANGLE95.0 DEGREES NOMINAL
CSMZLEFT TOP INSIDE ANGLE85.0 DEGREES NOMINAL
HEATHEAT TREATMENTANNEALED
MATLMATERIALTITANIUM ALLOY, MIL-T-81556, COMP AB-1
ZZZTNONDEFINITIVE SPEC/STD DATACOMPOSITION AB-1 AND CONDITION A
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