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NSN 5340-00-153-1011 (5340001531011) Bracket Angle Parts Catalog

The part belongs to NSN 5340-00-153-1011 is an Bracket Angle produced by United Technologies, Turbo Power Marine System, 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 5340-00-153-1011 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 Angle made by United Technologies, Turbo Power Marine System, Gould Inc Simulation Systems Div that carries the NSN 5340-00-153-1011, 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 5340001531011 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: 5340-00-153-1011
Item Name: Bracket Angle
FSG: 53 Hardware and Abrasives
Federal Supply Class (FSC): 5340 Hardware, Commercial
NCB Code: USA (00)
Manufacturers: Gould Inc Simulation Systems Div, Turbo Power Marine System, United Technologies

Manufacturer’s List for NSN 5340-00-153-1011

gould inc simulation systems div turbo power marine system united technologies

Part Number's List for NSN 5340-00-153-1011

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

Technical Characteristics of NSN 5340001531011

MRCCriteriaCharacteristic
ADLKFIRST LEG LENGTH1.307 INCHES NOMINAL
ADLLSECOND LEG LENGTH1.769 INCHES MINIMUM AND 1.779 INCHES MAXIMUM
AGAVEND ITEM IDENTIFICATIONW/S:ENGINE, AIRCRAFT, TF-33-P-7 (C-141A/B); ENGINE, AIRCRAFT TF33-PW-102 (C-135E, EC-135H/K/P); ENGINE, AIRCRAFT TF33-P-3/5/9 (C/EC-135, B-52H); ENGINE, AIRCRAFT TF-30
AHLKFIRST LEG HOLE DIAMETER0.216 INCHES MINIMUM AND 0.226 INCHES MAXIMUM
AHLNSECOND LEG HOLE DIAMETER0.276 INCHES MINIMUM AND 0.286 INCHES MAXIMUM
AHLPSECOND LEG DISTANCE BETWEEN HOLE CENTERS ALONG WIDTH1.173 INCHES NOMINAL
AHLVSECOND LEG DISTANCE FROM EDGE TO HOLE CENTER ALONG WIDTH0.250 INCHES NOMINAL
AHLWSECOND LEG DISTANCE FROM EDGE TO HOLE CENTER ALONG LENGTH0.200 INCHES MINIMUM AND 0.210 INCHES MAXIMUM
AHPWFIRST LEG THICKNESS0.056 INCHES MINIMUM AND 0.062 INCHES MAXIMUM
AHPXSECOND LEG THICKNESS0.056 INCHES MINIMUM AND 0.062 INCHES MAXIMUM
AHRAFIRST LEG DISTANCE FROM EDGE TO HOLE CENTER ALONG WIDTH0.250 INCHES NOMINAL
AHRBFIRST LEG DISTANCE FROM EDGE TO HOLE CENTER ALONG LENGTH0.250 INCHES NOMINAL
AJFPFIRST LEG END RADIUS0.250 INCHES NOMINAL
AJZUFIRST LEG STYLEEND RADIUS AND TAPERED
AKAUFIRST LEG HOLE ARRANGEMENT STYLEONE HOLE
AKCUSECOND LEG HOLE ARRANGEMENT STYLETWO HOLES
CSSQFIRST LEG ANGLE90.0 DEGREES NOMINAL
MATTMATERIALSTEEL COMP 410
MDCLMATERIAL DOCUMENT AND CLASSIFICATIONAMS 5504 ASSN STD SINGLE MATERIAL RESPONSE
STYLSTYLE DESIGNATORANGLE