9540-00-528-4798 (QQ-A-200/11, 2-1329, 1242517) Data

9540-00-528-4798 (9540005284798) NSN Information

NSNFSCNIINItem NameINC
9540-00-528-47989540005284798Angle, Structural37017

9540-00-528-4798 Features

MRCParameterCharacteristics
AARNFabrication MethodExtruded
ABKWOverall Height0.750 inches nominal
ABMKOverall Width1.000 inches nominal
ABRYLength10.000 feet minimum and 12.000 feet maximum
ADXLLeft Side Flange Thickness0.063 inches nominal
AGTABasic Shape StyleAngle
AJGLFillet Radius Where Left Flange Joins Base Flange0.125 inches nominal
AJGPBase Flange Thickness0.063 inches nominal
AJJBFirst TIP Radius0.063 inches nominal
BRFDWeight per Unit Measure0.130 pounds per linear foot
CMZYFirst TIP StyleRight quarter radius
CMZZSecond TIP Radius0.063 inches nominal
CNQJSecond TIP Relationship to First TIPNot identical
CNQKSecond TIP StyleUpper radius
CQHPLeft Inside Angle90.0 degrees nominal
HEATHeat TreatmentO-annealed
MATTMaterialAluminum alloy 7075
MDCLMaterial Document and ClassificationQQ-A-200/11 fed spec 1ST material response
ZZZTNondefinitive Spec/STD DataO temper

9540-00-528-4798 Manufacturing Part Numbers (SKUs)

MFG SKUCAGESTATUSISCRNVCRNCCSADCDACHCCRNAAC
124251718355A95 KZ
124251788277A15 KZ
1466214170R95 KZ
2-132938597A15 KZ
AND10134-100399237A14 KZ
QQ-A-200/1181348A14 KZ

9540-00-528-4798 Manufacturer

MFG SKUCAGEManufacturerTypeStatusRole
AND10134-100399237Airforce-Navy Aeronautical DesignMA
124251718355Boeing Company, TheAA
124251788277Boeing Company, TheAA
QQ-A-200/1181348Federal SpecificationsAA
1466214170Hughes Missile Systems Co.AR
2-132938597Lockheed Martin CorporationFA

9540-00-528-4798 FLIS Identification

PMICADPE CODECRITL CODEDEMIL CODEDEMIL INTGNIIN ASGMTESDHMICENACSCHEDULE_BINC
UXA01-JAN-1963N37017

9540-00-528-4798 Demilitarization Codes & Management

DMLPMICHMICADPECCriticalityESDC
AN

9540-00-528-4798 Non-consumable Item Support

MOE RULENIMSCDSOR
ZP01

9540-00-528-4798 Freight

NMFCNMFC SUBUFCHMCLTLLCLWCCTCCSHCADCACCASHNMF DESC
013140X05390S576ZRABZ