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NSN 5340-01-220-3137 (5340012203137) Bracket Double Angle Parts Catalog

The part belongs to NSN 5340-01-220-3137 is an Bracket Double Angle produced by United Technologies, Tokyo Judogi Kogyo Co, Parmac Inc, Instrument Support Inc, Gould Inc Simulation Systems Div. This specific NSN is a numeric identifier assigned by the Defense Logistics Agency (DLA) to categorize all products distributed by the NATO federal supply chain. At ASAP AOG, a company owned and operated by ASAP Semiconductor, we possess parts that belong to the NSN 5340-01-220-3137 and these are readily available in our current inventory. Our on-hand inventory contains parts belonging to this particular NSN that you can easily access. So, if you need an Bracket Double Angle made by United Technologies, Tokyo Judogi Kogyo Co, Parmac Inc, Instrument Support Inc, Gould Inc Simulation Systems Div that carries the NSN 5340-01-220-3137, you can rely on us to provide you with the necessary parts from our available inventory.


At ASAP AOG, we are dedicated to providing competitive quotes for premium NATO parts. We work hard to ensure all the national stock number 5340012203137 parts are fully certified and up to standard. Our supply chain is extensive and one of the fastest in the industry. Have a question or need a quote today? Simply fill out the RFQ below.


Alternative NSN: 5340-01-220-3137
Item Name: Bracket Double Angle
FSG: 53 Hardware and Abrasives
Federal Supply Class (FSC): 5340 Hardware, Commercial
NCB Code: USA (01)
Manufacturers: Gould Inc Simulation Systems Div, Instrument Support Inc, Parmac Inc, Tokyo Judogi Kogyo Co, United Technologies

Part Number's List for NSN 5340-01-220-3137

Part No.
Manufacturer
Item Name
Availability
RFQ
Bracket Double Angle
YES
RFQ
Bracket Double Angle
YES
RFQ
Bracket Double Angle
YES
RFQ
Bracket Double Angle
YES
RFQ
Bracket Double Angle
YES
RFQ

Technical Characteristics of NSN 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