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Quality guaranteed We sell only warrantied and traceable partsAt 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 446169, which is a Bracket Angle from manufacturer Turbo Power And Marine System Inc, 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 446169 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 Turbo Power And Marine System Inc parts from NSN 5340003442956, 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 446169 purchasing process instantly, submit an RFQ today.
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 5340-00-344-2956 Item Description: Bracket Angle | 5340 | 003442956 | 0 | P | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| U | U | |||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| 446169 | 2 | 9 | 5 |
| MRC | Criteria | Characteristic |
|---|---|---|
| AGAV | III END ITEM IDENTIFICATION | CASE ASSEMBLY,TURBINE; W/S: ENGINE, AIRCRAFT TF33-PW-102 (C-135E, EC-135H/K/P); ENGINE, AIRCRAFT, TF-33-P-7 (C-141A/B); AIRCRAFT, STRATOFORTRESS B-52; ENGINE, AIRCRAFT TF33-P-3/5/9 (C/EC-135, B-52H) |
| AHLF | SECOND LEG WIDTH | 1.509 INCHES NOMINAL |
| AHLG | SECOND LEG CORNER RADIUS | 0.250 INCHES NOMINAL |
| AHLK | FIRST LEG HOLE DIAMETER | 0.224 INCHES NOMINAL |
| AHLN | SECOND LEG HOLE DIAMETER | 0.286 INCHES NOMINAL |
| AHLP | SECOND LEG DISTANCE BETWEEN HOLE CENTERS ALONG WIDTH | 1.009 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 | 0.250 INCHES NOMINAL |
| AHPW | FIRST LEG THICKNESS | 0.062 INCHES NOMINAL |
| AHPX | SECOND LEG THICKNESS | 0.062 INCHES NOMINAL |
| AHQN | FIRST LEG WIDTH | 0.510 INCHES NOMINAL |
| 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 | 0.375 INCHES NOMINAL |
| AJZU | FIRST LEG STYLE | END RADIUS |
| AKAU | FIRST LEG HOLE ARRANGEMENT STYLE | ONE HOLE |
| AKBU | SECOND LEG STYLE | CORNER RADIUS |
| AKCU | SECOND LEG HOLE ARRANGEMENT STYLE | TWO HOLES |
| CSSP | SECOND LEG RELATIONSHIP TO FIRST LEG | NOT IDENTICAL |
| CSSQ | FIRST LEG ANGLE | 130.0 DEGREES NOMINAL |
| CSSZ | SECOND LEG OFFSET ANGLE | 80.9 DEGREES NOMINAL |
| MATT | MATERIAL | STEEL COMP 410 |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | 66 FED STD SINGLE MATERIAL RESPONSE |
| STYL | STYLE DESIGNATOR | OFFSET ANGLE |
| ZZZV | III FSC APPLICATION DATA | ENGINE,JET,AIRCRAFT |
 |
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