At Aviation Parts Circuit, we offer an unparalleled selection of parts for the aerospace, civil aviation, defense, electronics, and IT hardware markets. Owned and operated by ASAP Semiconductor, we have access to an inventory of more than two billion new and obsolete parts organized into an efficient, streamlined, and easy-to-navigate purchasing platform. Part numbers such as 676331, which is a Bracket Angle from manufacturer Gould E A And Co, are in stock and ready to ship with short lead times and competitive prices. We specialize in leveraging our purchasing power with major suppliers, allowing us to offer lower costs and faster shipping on all orders, even in AOG situations. Our team at Aviation Parts Circuit is available 24/7x365 to provide you with a quick quotation on part 676331 and any other NSN part listed on our website.
To help users quickly locate the parts they need, our website offers a broad scope of parametric search measures, allowing customers to filter parts by their Federal Supply Group or Class, part type, part family, CAGE Code, NSN, and more. For example, if you are in need of Gould E A And Co parts from NSN 5340001531011, our website can provide you with a selection of parts exclusively from that manufacturer and NSN. At Aviation Parts Circuit, our goal is not only to improve the parts procurement process, but to revolutionize it entirely. To begin the NSN part 676331 purchasing process instantly, submit an RFQ today.
NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
5340-00-153-1011 Item Description: Bracket Angle | 5340 | 001531011 | 0 | P | ||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
U | U | |||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
676331 | 2 | 2 | 3 |
MRC | Criteria | Characteristic |
---|---|---|
ADLK | FIRST LEG LENGTH | 1.307 INCHES NOMINAL |
ADLL | SECOND LEG LENGTH | 1.769 INCHES MINIMUM AND 1.779 INCHES MAXIMUM |
AGAV | END ITEM IDENTIFICATION | W/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 |
AHLK | FIRST LEG HOLE DIAMETER | 0.216 INCHES MINIMUM AND 0.226 INCHES MAXIMUM |
AHLN | SECOND LEG HOLE DIAMETER | 0.276 INCHES MINIMUM AND 0.286 INCHES MAXIMUM |
AHLP | SECOND LEG DISTANCE BETWEEN HOLE CENTERS ALONG WIDTH | 1.173 INCHES NOMINAL |
AHLV | SECOND LEG DISTANCE FROM EDGE TO HOLE CENTER ALONG WIDTH | 0.250 INCHES NOMINAL |
AHLW | SECOND LEG DISTANCE FROM EDGE TO HOLE CENTER ALONG LENGTH | 0.200 INCHES MINIMUM AND 0.210 INCHES MAXIMUM |
AHPW | FIRST LEG THICKNESS | 0.056 INCHES MINIMUM AND 0.062 INCHES MAXIMUM |
AHPX | SECOND LEG THICKNESS | 0.056 INCHES MINIMUM AND 0.062 INCHES MAXIMUM |
AHRA | FIRST LEG DISTANCE FROM EDGE TO HOLE CENTER ALONG WIDTH | 0.250 INCHES NOMINAL |
AHRB | FIRST LEG DISTANCE FROM EDGE TO HOLE CENTER ALONG LENGTH | 0.250 INCHES NOMINAL |
AJFP | FIRST LEG END RADIUS | 0.250 INCHES NOMINAL |
AJZU | FIRST LEG STYLE | END RADIUS AND TAPERED |
AKAU | FIRST LEG HOLE ARRANGEMENT STYLE | ONE HOLE |
AKCU | SECOND LEG HOLE ARRANGEMENT STYLE | TWO HOLES |
CSSQ | FIRST LEG ANGLE | 90.0 DEGREES NOMINAL |
MATT | MATERIAL | STEEL COMP 410 |
MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | AMS 5504 ASSN STD SINGLE MATERIAL RESPONSE |
STYL | STYLE DESIGNATOR | ANGLE |
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