Part Number ST9M580AC1R with NSN 5340011056679 by Boeing Company The - Request for Quote Now!

Part Number: ST9M580AC1R
Manufacturer: Boeing Company The
NIIN: 011056679
Item Name : Bracket Angle
CAGE Code: 76301
FSG: 53 Hardware and Abrasives
Country: USA
NCB Code: 01

Whether you are in search of military and defense parts, aerospace parts, or other similar product solutions, Satellite To Submarine Parts is your one-stop shop. Thank you for your interest in part number ST9M580AC1R, a Boeing Company The item that is listed alongside the description “Bracket Angle” and the NSN 5340011056679. To guarantee a swift procurement process for NSN part number ST9M580AC1R, be sure to request a quote by filling out and submitting the RFQ form below, and one of our experts will offer a customized solution for your comparisons in response.

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We list everything with as much relevant information as possible to ensure that customers can swiftly identify and procure the exact products they need. For instance, while part number ST9M580AC1R is manufactured by Boeing Company The, it is specifically done so under CAGE Code 76301, a unique identifier assigned to a particular facility by the DLA that supplies to various government or defense agencies. Additionally, using the first digits of the NSN 5340-01-105-6679, one can also determine that this part falls under FSC 5340 Hardware Commercial. Keeping this in mind, initiate the purchasing process today to see why so many customers depend on us for the NSN items they require.

NSN Information for Part Number ST9M580AC1R with NSN 5340-01-105-6679, 5340011056679

NSNFSCNIINCLSHazmatDEMILCancelled NSN
5340-01-105-6679

Item PartTypeName:

BRACKET,ANGLE

53400110566790P
CIICHCCESDPMICCriticalityENAC
UA0
Part NumberISCRNVCRNCCHCCMSDSSADC
ST9M580C1R595

Characteristics Data of NSN 5340-01-105-6679, 5340011056679

MRCCriteriaCharacteristic
ADLKFIRST LEG LENGTH0.750 INCHES NOMINAL
ADLLSECOND LEG LENGTH0.750 INCHES NOMINAL
AGAVEND ITEM IDENTIFICATIONW/S: AIRCRAFT,HARRIER AV-8B; AIRCRAFT,EAGLE F-15; AIRCRAFT,HORNET F/A-18; F/A-18E/F HORNET AIRCRAFT; AVIATION ORDANCE; GUN SYSTEM,25MM
AHLFSECOND LEG WIDTH0.980 INCHES MINIMUM AND 1.020 INCHES MAXIMUM
AHLGSECOND LEG CORNER RADIUS0.220 INCHES MINIMUM AND 0.280 INCHES MAXIMUM
AHLKFIRST LEG HOLE DIAMETER0.129 INCHES MINIMUM AND 0.134 INCHES MAXIMUM
AHLNSECOND LEG HOLE DIAMETER0.220 INCHES MINIMUM AND 0.230 INCHES MAXIMUM
AHLVSECOND LEG DISTANCE FROM EDGE TO HOLE CENTER ALONG WIDTH0.230 INCHES MINIMUM AND 0.250 INCHES MAXIMUM
AHLWSECOND LEG DISTANCE FROM EDGE TO HOLE CENTER ALONG LENGTH0.220 INCHES MINIMUM AND 0.280 INCHES MAXIMUM
AHPWFIRST LEG THICKNESS0.050 INCHES NOMINAL
AHPXSECOND LEG THICKNESS0.050 INCHES NOMINAL
AHQNFIRST LEG WIDTH0.980 INCHES MINIMUM AND 1.020 INCHES MAXIMUM
AHQPFIRST LEG CORNER RADIUS0.220 INCHES MINIMUM AND 0.280 INCHES MAXIMUM
AHQUFIRST LEG DISTANCE BETWEEN HOLE CENTERS ALONG WIDTH0.490 INCHES MINIMUM AND 0.510 INCHES MAXIMUM
AHRAFIRST LEG DISTANCE FROM EDGE TO HOLE CENTER ALONG WIDTH0.240 INCHES MINIMUM AND 0.260 INCHES MAXIMUM
AHRBFIRST LEG DISTANCE FROM EDGE TO HOLE CENTER ALONG LENGTH0.220 INCHES MINIMUM AND 0.280 INCHES MAXIMUM
AJZUFIRST LEG STYLECORNER RADIUS
AKAUFIRST LEG HOLE ARRANGEMENT STYLETWO HOLES
AKBUSECOND LEG STYLECORNER RADIUS
AKCUSECOND LEG HOLE ARRANGEMENT STYLETWO HOLES
CSSPSECOND LEG RELATIONSHIP TO FIRST LEGNOT IDENTICAL
CSSQFIRST LEG ANGLE90.0 DEGREES NOMINAL
MATTMATERIALALUMINUM ALLOY 2024
MDCLMATERIAL DOCUMENT AND CLASSIFICATIONQQ-A-250/5,T81 FED SPEC SINGLE MATERIAL RESPONSE
SFTTSURFACE TREATMENTPAINT
STDCSURFACE TREATMENT DOCUMENT AND CLASSIFICATIONMIL-P-23377 MIL SPEC SINGLE TREATMENT RESPONSE
STYLSTYLE DESIGNATORANGLE

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