9540-00-261-5159 (PA6582, 5781, 24826) Data

9540-00-261-5159 (9540002615159) NSN Information

NSNFSCNIINItem NameINC
9540-00-261-51599540002615159Beam, Structural37018

9540-00-261-5159 Features

MRCParameterCharacteristics
AARNFabrication MethodExtruded
ABKWOverall Height1.250 inches nominal
ABRYLength10.000 feet minimum and 12.000 feet maximum
ADXRLeft Side Top Flange Thickness0.063 inches nominal
ADXSRight Side Top Flange Thickness0.063 inches nominal
AGTABasic Shape StyleT shape
AJJPLeg Thickness0.063 inches nominal
BPXDLeft Side Top Flange Distance to Center of Both Flanges0.750 inches nominal
BPXGRight Side Top Flange Distance to Center of Both Flanges0.750 inches nominal
BPXJFillet Radius Where Top Left Flange Joins Web Flange/Leg0.063 inches nominal
BPXLFillet Radius Where Top Right Flange Joins Web Flange/Leg0.063 inches nominal
BQJGTop Flange Width1.500 inches nominal
BRFDWeight per Unit Measure0.210 pounds per linear foot
CMZYFirst TIP StyleSquare end
CNQJSecond TIP Relationship to First TIPIdentical
CNQLThird TIP Relationship to Preceding TipsIdentical W/first tip
CRZCRight Top Inside Angle90.0 degrees nominal
CSMZLeft Top Inside Angle90.0 degrees nominal
HEATHeat TreatmentT-6 solution heat treated
MATLUnable to DecodeUnable to decode
MATTMaterialAluminum alloy AMS-QQ-A-200/11, alloy 7075
ZZZTNondefinitive Spec/STD DataT6 temper

9540-00-261-5159 Manufacturing Part Numbers (SKUs)

MFG SKUCAGESTATUSISCRNVCRNCCSADCDACHCCRNAAC
13487-327610F95 KZ
13763-327610F95 KZ
2-228238597A13 KZ
2482601634Y13 KZ
578101484H95 KZ
60-312929321A13 KZ
AMS-QQ-A-200/110U583A13 ZZ
AMS-QQ-A-200/1181343R95 ZZ
E7122020WLU1F95 KZ
E71220214170R95 KZ
E7122027B709R95 KZ
PA658206012F95 KZ
QQ-A-200/1181348A95 KZ

9540-00-261-5159 Manufacturer

MFG SKUCAGEManufacturerTypeStatusRole
2482601634Aluminum Co. of AmericaAY
QQ-A-200/1181348Federal SpecificationsAA
E7122020WLU1General Dynamics Corp.AF
E71220214170Hughes Missile Systems Co.AR
13487-327610International Light Metals Corp.AF
13763-327610International Light Metals Corp.AF
2-228238597Lockheed Martin CorporationFA
578101484Reynolds Metals Co.AH
AMS-QQ-A-200/110U583SAE InternationalCA
AMS-QQ-A-200/1181343Society of Automotive Engineers Inc.AR
E7122027B709Tracor Flight Systems Inc.AR
60-312929321Transtar Metals Corp.AA
PA658206012Transtar Metals Corp.FF

9540-00-261-5159 Replaces the Following Cancelled NSN

Cancelled NSNCancelled NIIN
9540-00-809-0702008090702

9540-00-261-5159 FLIS Identification

PMICADPE CODECRITL CODEDEMIL CODEDEMIL INTGNIIN ASGMTESDHMICENACSCHEDULE_BINC
A0XA101-JAN-1963N761090004037018

9540-00-261-5159 FLIS Management

MOEREC REP CODEMGMT CTLUSCPHRASE CODEPHRASE STATEMENT
DSN-------I
DFNSF9---VF

9540-00-261-5159 Demilitarization Codes & Management

DMLPMICHMICADPECCriticalityESDC
AN0X

9540-00-261-5159 Miscellaneous Management

MOE (S_A)SOSAACQUPUISLCCIICRCMCCSVC
DFSMSJ1FT0UNSF9---VF
DFSMSJ1FT0UNSF9---VI
DSSMSJ1FT0UN-------F
DSSMSJ1FT0UN-------I

9540-00-261-5159 Component / End Item

WPN SYS IDWPN SYS SVCWEAPON SYSTEM
06FAircraft, Hercules C-130

9540-00-261-5159 Non-consumable Item Support

MOE RULENIMSCDSOR
FGGI
ZI01

9540-00-261-5159 Management Control Air Force

FUNDBUDGETMMACPVC
SF9V

9540-00-261-5159 Freight

NMFCNMFC SUBUFCHMCLTLLCLWCCTCCSHCADCACCASHNMF DESC
104420X53800U576Z9ABZ

9540-00-261-5159 FLIS Packaging 1

PICA SICATOSICQMOPCLNG DRYINGPRES MATWRAP MATPKG CATPKG DESIGN ACTYCUSH DUN
PB000ZZ1ZZZZ37ZZZZ

9540-00-261-5159 FLIS Packaging 2

THKUNIT CONTPKG DATA SOURCEINTER CONTUCLSPC MKGLVL ALVL BLVL C
C00P00Z

9540-00-261-5159 FLIS Packaging 3

UNIT PACK WEIGHTUNIT PACK SIZEUNIT PACK CUBECONT NSNOPIUNPKG ITEM DIMUNPKG ITEM WEIGHTSPI DATESPI NOSPI REVSUPPL INSTR
0000.20000.013MPRESERVATION ZZ = IAW AST