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 4028800, which is a Bracket Angle from manufacturer United Technologies Corporation, 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 4028800 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 United Technologies Corporation parts from NSN 5340003859275, 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 4028800 purchasing process instantly, submit an RFQ today.
NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
5340-00-385-9275 Item Description: Bracket Angle | 5340 | 003859275 | 0 | P | ||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
U | U | |||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
4028800 | 6 | 9 | 5 |
MRC | Criteria | Characteristic |
---|---|---|
AGAV | END ITEM IDENTIFICATION | W/S:ENGINE, AIRCRAFT, F100 PW220 (F-15C/D/E); ENGINE, AIRCRAFT, F100-PW-100 (F-15A/B/C/D); AIRCRAFT, EAGLE F-15; SUPPORT EQUIPMENT, C-5 AIRCRAFT; ENGINE, AIRCRAFT, F100-PW-200 (F-16A/B/C/D); AIRCRAFT, F-16 |
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 |
AHLS | SECOND LEG DISTANCE BETWEEN HOLE CENTERS ALONG LENGTH | 1.500 NOMINAL INCHES |
AHLV | SECOND LEG DISTANCE FROM EDGE TO HOLE CENTER ALONG WIDTH | 0.640 INCHES NOMINAL |
AHPW | FIRST LEG THICKNESS | 0.045 INCHES MINIMUM AND 0.055 INCHES MAXIMUM |
AHPX | SECOND LEG THICKNESS | 0.045 INCHES MINIMUM AND 0.055 INCHES MAXIMUM |
AJZU | FIRST LEG STYLE | END RADIUS |
AKAU | FIRST LEG HOLE ARRANGEMENT STYLE | ONE HOLE |
AKCU | SECOND LEG HOLE ARRANGEMENT STYLE | TWO HOLES |
CSSP | SECOND LEG RELATIONSHIP TO FIRST LEG | NOT IDENTICAL |
CSSQ | FIRST LEG ANGLE | 0.109 RADIANS MINIMUM AND 0.141 RADIANS MAXIMUM |
MATT | MATERIAL | TITANIUM ALLOY |
MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | AMS 4911 NATIONAL SPEC SINGLE MATERIAL RESPONSE |
STYL | STYLE DESIGNATOR | OFFSET ANGLE |
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