INSTANT RFQ

4061734 of United Technologies Corporation under NSN 5340-01-220-3137

Part Number: 4061734
NIIN: 012203137
Item Name : Bracket Double Angle
CAGE Code: 77445
FSG: 53 Hardware and Abrasives
Country: USA
NCB Code: 01

Thank you for taking an interest in our selection of 5340-01-220-3137 parts here on Boost AOG. You are currently on the RFQ form for part number 4061734, a United Technologies Corporation product listed with the Bracket Double Angle If part number 4061734 catches your eye, be sure to use our online RFQ service to request quotes, with customized responses provided within 15 minutes of us receiving and reviewing a completed submission.

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To ensure the quality of our NSN components, we adhere to a strict NO CHINA SOURCING pledge, meaning every purchased item will be delivered alongside any pertinent qualifying certifications or manufacturing trace documentation for your benefit. Paired with numerous other commitments, we proudly operate with AS9120B, ISO 9001:2015, and FAA AC 00-56B accreditation. If you happen to be facing a time constraint and require NSN parts quickly, contact us at your earliest convenience, and we will discuss the expedited shipping options we have available for domestic and international customers alike. With our various dedications in mind, kick off procurement for United Technologies Corporation part number 4061734 and other Bracket Double Angle products today.

NSN Information for Part Number 4061734 with NSN 5340-01-220-3137, 5340012203137

NSNFSCNIINCLSHazmatDEMILCancelled NSN
5340-01-220-3137

Item PartTypeName:

BRACKET,DOUBLE ANGLE

53400122031370P
CIICHCCESDPMICCriticalityENAC
UA
Part NumberISCRNVCRNCCHCCMSDSSADC
4061734623

Characteristics Data of NSN 5340-01-220-3137, 5340012203137

MRCCriteriaCharacteristic
ACHYMOUNTING HOLE TYPEPLAIN
ADLKFIRST LEG LENGTH0.638 INCHES NOMINAL
ADLLSECOND LEG LENGTH0.765 INCHES NOMINAL
AGAVEND ITEM IDENTIFICATIONW/S:ENGINE,AIRCRAFT,F100 PW220 (F-15C/D/E); ENGINE,AIRCRAFT,F100-PW-100 (F-15A/B/C/D); SUPPORT EQUIPMENT,C-5 AIRCRAFT; AIRCRAFT,EAGLE F-15; ENGINE,AIRCRAFT,F100-PW-200 (F-16A/B/C/D)
AHLFSECOND LEG WIDTH1.670 INCHES NOMINAL
AHLGSECOND LEG CORNER RADIUS0.150 INCHES NOMINAL
AHLNSECOND LEG HOLE DIAMETER0.261 INCHES MINIMUM AND 0.271 INCHES MAXIMUM
AHLPSECOND LEG DISTANCE BETWEEN HOLE CENTERS ALONG WIDTH1.158 INCHES NOMINAL
AHLVSECOND LEG DISTANCE FROM EDGE TO HOLE CENTER ALONG WIDTH0.256 INCHES NOMINAL
AHLWSECOND LEG DISTANCE FROM EDGE TO HOLE CENTER ALONG LENGTH0.188 INCHES NOMINAL
AHPWFIRST LEG THICKNESS0.037 INCHES MINIMUM AND 0.044 INCHES MAXIMUM
AHPXSECOND LEG THICKNESS0.037 INCHES MINIMUM AND 0.044 INCHES MAXIMUM
AHPZCENTER SECTION HEIGHT1.405 INCHES NOMINAL
AHQACENTER SECTION WIDTH1.670 INCHES NOMINAL
AHQBCENTER SECTION THICKNESS0.037 INCHES MINIMUM AND 0.044 INCHES MAXIMUM
AHQNFIRST LEG WIDTH1.670 INCHES NOMINAL
AHQPFIRST LEG CORNER RADIUS0.250 INCHES NOMINAL
AJZUFIRST LEG STYLECORNER RADIUS
AKAUFIRST LEG HOLE ARRANGEMENT STYLENO HOLE
AKBUSECOND LEG STYLECORNER RADIUS
AKCUSECOND LEG HOLE ARRANGEMENT STYLETWO HOLES
CSSPSECOND LEG RELATIONSHIP TO FIRST LEGNOT IDENTICAL
CSSQFIRST LEG ANGLE149.7 DEGREES NOMINAL
CSSRSECOND LEG ANGLE149.7 DEGREES NOMINAL
FEATSPECIAL FEATURESCENTER OF FIRST LEG RADIUSED INWARD 0.750 IN.
MATTMATERIALNICKEL ALLOY X-750
MDCLMATERIAL DOCUMENT AND CLASSIFICATIONAMS 5542 ASSN STD SINGLE MATERIAL RESPONSE
STYLSTYLE DESIGNATORDOUBLE ANGLE

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